| 编号 | 中文名称 | 英文名称 |
|---|---|---|
| ISO 10096-1997 | 航空航天.等级为:450 MPa(环境温度)/425℃、600 MPa(环境温度)/235℃、600 MPa(环境温度)/315℃、600 MPa( | Aerospace - Nuts, hexagonal, slotted (castellated), reduced height, reduced across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/425 °C, 600 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/315 °C, 600 MPa (at ambient temperature)/650 °C, 900 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature) /730 °C and 1100 MPa (at ambiente temperature)/600 °C - Dimensions |
| ISO 1022-1988 | 航空航天 流体系统用气态氧充气接头(旧型) 尺寸(英制系列) | Aerospace; gaseous oxygen replenishment connection for use in fluid systems (old type); dimensions (inch series) |
| ISO 10299-2000 | 航空航天 实心铆钉 材料和米制的识别 | Aerospace - Rivets, solid - Material and metric series identification |
| ISO 10502-1992 | 航空航天.温度为230℃及以下、压力为10500 kPa下使用的聚四氟乙烯(PTFE)软管组件.采购规范 | Aerospace; hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10500 kPa; procurement specification |
| ISO 10583-1993 | 航空航天 流体系统 导管/组件试验方法 | Aerospace fluid systems; test methods for tube/fitting assemblies |
| ISO 10792-1-1995 | 航空航天 飞机结构用不锈钢自润滑球面滑动轴承 第1部分:米制系列 | Aerospace - Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner - Part 1: Metric series |
| ISO 10792-2-1995 | 航空航天 飞机结构用不锈钢自润滑球面滑动轴承 第2部分:英制系列 | Aerospace - Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner - Part 2: Inch series |
| ISO 10792-3-1995 | 航空航天 飞机结构用不锈钢自润滑球面滑动轴承 第3部分:技术规范 | Aerospace - Airframe spherical plain bearings in corrosion-resisting steel with self-lubricating liner - Part 3: Technical specification |
| ISO 10955-1999 | 航空航天 航空器操纵钢丝绳用末端接头和松紧套筒 技术规范 | Aerospace - End-fittings and turnbarrels for aircraft control wire rope - Technical specification |
| ISO 10959-2000 | 航空航天 MJ螺纹 量规 | Aerospace - MJ threads - Gauging |
| ISO 11077-1993 | 航空航天 自行式除冰和防冰车 功能要求 | Aerospace; self-proppelled de-icing/anti-icing vehicles; functional requirements |
| ISO 11217-1993 | 航空航天 液压系统液体污染物 取样点位置和取样准则 | Aerospace; hydraulic system fluid contamination; location of sampling points and citeria for sampling |
| ISO 11218-1993 | 航空航天 液压油液清洁度分级 | Aerospace; cleanliness classification for hydraulic fluids |
| ISO 12-1987 | 航空航天 管路 识别标志 | Aerospace; Pipelines; Identification |
| ISO 12256-2002 | 航空航天.内十字形槽扳手.米制系列 | Aerospace - Drives, internal, cruciform, ribbed - Metric series |
| ISO 12258-1998 | 航空航天 强度等级小于或等于1275MPa、金属材料制成、有涂覆或未涂覆、具有长MJ螺纹及大径或中径杆型的双六 | Aerospace - Bolts, reduced bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1275 MPa - Dimensions |
| ISO 12260-1996 | 航空航天 强度等级小于或等于1100MPa、金属材料制成、有涂覆或未涂覆、短的或中等长度MJ螺纹,阶梯杆型、内 | Aerospace - Screws, pan head, internal offset cruciform ribbed or unripped drive, stepped shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa - Dimensions |
| ISO 12261-1996 | 航空航天 强度等级小于或等于1100MPa、金属材料制成、有涂覆或未涂覆、长长度MJ螺纹、中径杆型、内偏高扭矩 | Aerospace - Screws, pan head, internal offset cruciform ribbed or unripped drive, pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa - Dimensions |
| ISO 12268-1997 | 航空航天.等级为:450 MPa(环境温度)/425℃、600 MPa(环境温度)/235℃、600 MPa(环境温度)/315℃、600 MPa( | Aerospace - Nuts, hexagonal, plain, reduced height, reduced across flats, with MJ threads; classifications: 450 MPa (at ambient temperature)/425 °C, 600 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/315 °C, 600 MPa (at ambient temperature)/650 °C, 900 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/730 °C and 1100 MPa (at ambiante temperature)/600 °C - Dimensions |
| ISO 12272-1998 | 航空航天.等级为:900 MPa(环境温度)/235℃、900 MPa(环境温度)/315℃和900 MPa(环境温度)/425℃,带增大沉孔 | Aerospace - Nuts, anchor, self-locking, floating, two lug, with incremental counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/315 °C and 900 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 12273-1997 | 航空航天.等级为:900 MPa(环境温度)/235℃、900 MPa(环境温度)/315℃和900 MPa(环境温度)/425℃,带MJ螺纹自 | Aerospace - Nuts, anchor, self-locking, floating, self-aligning, two lug, with MJ threads; classifications: 900 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/315 °C and 900 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 12274-1997 | 航空航天.等级为:900 MPa(环境温度)/235℃、900 MPa(环境温度)/315℃、900 MPa(环境温度)/425℃,带MJ螺纹自 | Aerospace - Nuts, anchor, self-locking, floating, self-aligning, single lug, with MJ threads; classifications: 900 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/315 °C and 900 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 12277-2000 | 航空航天 等级为:1100 MPa(环境温度)/120℃、1100 MPa(环境温度)/235℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Gang channel, self-locking, floating, standard series, with counterbore, classifications: 1100 MPa (at ambient temperature)/120 °C, 1100 MPa (at ambient temperature)/235 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 12278-1999 | 航空航天.等级为:900 MPa(环境温度)/235℃、1100 MPa(环境温度)/235℃、1250 MPa(环境温度)/235℃和550 MPa | Aerospace - Nuts, barrel, self-locking, floating, self-aligning, with MJ threads, classifications: 900 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/235 °C, 1250 MPa (at ambient temperature)/235 °C and 1550 MPa (at ambient temperature)/235 °C - Dimensions |
| ISO 12280-1999 | 航空航天 筒形自锁螺母用弹性金属片保持架 尺寸 | Aerospace - Retainers, spring, sheet metal, for self-locking barrel nuts - Dimensions |
| ISO 12281-1999 | 航空航天.经过或未经过表面处理的金属材料制100°普通沉头实心铆钉.尺寸 | Aerospace - Rivets, solid, 100° normal countersunk head, in metallic material, with or without surface treatment - Dimensions |
| ISO 12288-2000 | 航空航天 镍合金实心铆钉 采购规范 | Aerospace - Rivets, solid, in nickel alloy - Procurement specification |
| ISO 12289-2003 | 航空航天.防腐蚀钢制实心铆钉.采购规范 | Aerospace - Rivets, solid, in corrosion-resisting steel - Procurement specification |
| ISO 12290-2000 | 航空航天 钛和钛合金实心铆钉 采购规范 | Aerospace - Rivets, solid, in titanium or titanium alloy - Procurement specification |
| ISO 12319-2006 | 航空航天. 'P'(环形)夹具.获取规范 | Aerospace - 'P' (loop style) clamps - Procurement specification |
| ISO 12333-2000 | 航空航天 连续置换液压马达 35000 kPa系统的一般规范 | Aerospace - Constant-displacement hydraulic motors - General specifications for 35000 kPa systems |
| ISO 12334-2000 | 航空航天 带压力补偿的变流量液压泵 35000 kPa系统的一般要求 | Aerospace - Hydraulic, pressure-compensated, variable delivery pumps - General requirements for 35000 kPa systems |
| ISO 13411-1997 | 航空航天 飞机结构用滚针、滚柱和滚道式滚子轴承 技术规范 | Aerospace - Airframe needle roller, cylindrical roller and track roller bearings - Technical specification |
| ISO 13412-1997 | 航空航天 飞机结构用轭型单列密封的滚针滚道式滚子 英制系列 | Aerospace - Airframe needle track roller, yoke type, single-row, sealed - Inch series |
| ISO 13413-1997 | 航空航天 飞机结构用轭型、双列密封的滚针滚道式滚子 英制系列 | Aerospace - Airframe needle track roller, yoke type, double-row, sealed - Inch series |
| ISO 13414-1997 | 航空航天 飞机结构用带档边的单列滚针轴承 英制系列 | Aerospace - Airframe needle roller bearings, single-row, shielded - Inch series |
| ISO 13415-1997 | 航空航天 飞机结构用柱型单列密封的滚针滚道式滚子 英制系列 | Aerospace - Airframe needle track roller, stud type, single-row, sealed - Inch series |
| ISO 13416-1997 | 航空航天 飞机结构用轭型单列密封的滚针滚道式滚子 米制系列 | Aerospace - Airframe needle track roller, yoke type, single-row, sealed - Metric series |
| ISO 13417-1997 | 航空航天 飞机结构用柱型单列密封的滚针滚道式滚子 米制系列 | Aerospace - Airframe needle track roller, stud type, single-row, sealed - Metric series |
| ISO 13589-1998 | 航空航天.等级:1100 MPa(环境温度)/425℃、1100 MPa(环境温度)/650℃、1210 MPa(环境温度)/425℃、1210 MPa | Aerospace - Nuts, bihexagonal, self-locking, with counterbore and MJ threads, classifications: 1100 MPa (at ambient temperature)/425 °C, 1100 MPa (at ambient temperature)/650 °C, 1210 MPa (at ambient temperature)/425 °C, 1210 MPa (at ambient temperature)/730 °C, 1550 MPa (at ambient temperature)/235 °C, 1550 MPa (at ambient temperature)/425 °C and 1550 MPa (at ambient temperature)/600° C - Dimensions |
| ISO 13595-2000 | 航空航天 涂覆或未涂覆、金属材料制、带MJ螺纹游动自锁螺母的螺纹衬套 尺寸 | Aerospace - Inserts, with self-locking floating nut, with MJ threads, in metallic material, coated or uncoated - Dimensions |
| ISO 13596-2000 | 航空航天 涂覆或未涂覆、金属材料制、带MJ螺纹的封闭型自锁螺纹衬套 尺寸 | Aerospace - Inserts, self-locking, with MJ threads, closed type, in metallic material, coated or uncoated - Dimensions |
| ISO 13597-2000 | 航空航天 涂覆或未涂覆、金属材料制、带MJ螺纹的开放型自锁螺纹衬套 尺寸 | Aerospace - Inserts, self-locking, with MJ threads, open type, in metallic material, coated or uncoated - Dimensions |
| ISO 13598-2000 | 航空航天 涂覆或未涂覆、金属材料制、缩减法兰、带MJ螺纹的封闭型自锁螺纹衬套 尺寸 | Aerospace - Inserts, self-locking, with MJ threads, reduced flanges, closed type, in metallic material, coated or uncoated - Dimensions |
| ISO 13599-2000 | 航空航天 涂覆或未涂覆、金属材料制、带间隙配合孔的螺纹衬套 尺寸 | Aerospace - Inserts, with clearance hole, in metallic material, coated or uncoated - Dimensions |
| ISO 13921-1996 | 航空航天.金属材料制涂覆或未涂覆的、强度等级小于或等于1100 MPa、具有大径杆型、短的和中等长度MJ螺纹、 | Aerospace - Screws, 100° reduced countersunk head, internal offset cruciform ribbed or unribbed drive, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa - Dimensions |
| ISO 14190-1998 | 航空航天 飞机结构用滚动轴承:滚珠和球面滚子轴承 技术规范 | Aerospace - Airframe rolling bearings: Ball and spherical roller bearings - Technical specification |
| ISO 14191-1998 | 航空航天 飞机结构用直径系列3和4的单列自位球面滚子轴承 米制系列 | Aerospace - Airframe spherical roller bearings, single-row, self-aligning, diameter series 3 and 4 - Metric series |
| ISO 14192-1998 | 航空航天 飞机结构用单列自位中等负荷防尘球面滚子轴承 米制系列 | Aerospace - Airframe spherical roller bearings, single row, self-aligning, shielded, intermediate duty - Metric series |
| ISO 14193-1998 | 航空航天 飞机结构用中等负荷扩展内圈单列自位密封球面滚子轴承 英制系列 | Aerospace - Airframe spherical roller bearings, single-row, self-aligning, sealed, extended inner ring, intermediate duty - Inch series |
| ISO 14194-1998 | 航空航天 飞机结构用重负荷扩展内圈自位双列密封球面滚子轴承 英制系列 | Aerospace - Airframe spherical roller bearings, double-row, self-aligning, sealed, extended inner ring, heavy duty - Inch series |
| ISO 14195-1998 | 航空航天 飞机结构用轻负荷扭力管设计的自位双列密封球面滚子轴承 英制系列 | Aerospace - Airframe spherical roller bearings, double-row, self-aligning, sealed, torque tube design, light duty - Inch series |
| ISO 14196-1998 | 航空航天 飞机结构用重负荷普通内圈自位双列密封球面滚子轴承 英制系列 | Aerospace - Airframe spherical roller bearings, double-row, self-aligning, sealed, plain inner ring, heavy duty - Inch series |
| ISO 14197-1998 | 航空航天 飞机结构用中等负荷自位单列密封球面滚子轴承 英制系列 | Aerospace - Airframe spherical roller bearings, single-row, self-aligning, sealed, intermediate duty - Inch series |
| ISO 14201-1998 | 航空航天 飞机结构用直径系列2的自位双列球轴承 米制系列 | Aerospace - Airframe ball bearings, double-row, self-aligning, diameter series 2 - Metric series |
| ISO 14202-1998 | 航空航天 飞机结构用直径系列0和2的单列刚性球轴承 米制系列 | Aerospace - Airframe ball bearings, single-row, rigid, diameter series 0 and 2 - Metric series |
| ISO 14203-1998 | 航空航天 飞机结构用直径系列8和9单列刚性球轴承 米制系列 | Aerospace - Airframe ball bearings, single-row, rigid, diameter series 8 and 9 - Metric series |
| ISO 14204-1998 | 航空航天 飞机结构用直径系列0的双列刚性球轴承 米制系列 | Aerospace - Airframe ball bearings, double-row, rigid, diameter series 0 - Metric series |
| ISO 14206-1998 | 航空航天 飞机结构用轻负荷单列刚性密封球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, sealed, light duty - Inch series |
| ISO 14207-1998 | 航空航天 飞机结构用轻负荷密封精密单列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, precision, sealed, light duty - Inch series |
| ISO 14208-1998 | 航空航天 飞机结构用中等负荷密封单列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, sealed, intermediate duty - Inch series |
| ISO 14209-1998 | 航空航天 飞机结构用中等负荷密封精密单列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, precision, sealed, intermediate duty - Inch series |
| ISO 14210-1998 | 航空航天 飞机结构用扭力管设计的轻负荷密封单列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, sealed, torque tube design, light duty - Inch series |
| ISO 14211-1998 | 航空航天 飞机结构用轻负荷扭力管设计的单列刚性密封精密球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, precision, sealed, torque tube design, light duty - Inch series |
| ISO 14212-1998 | 航空航天 飞机结构用扭力管设计的超轻负荷密封单列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, sealed, torque tube design, extra-light duty - Inch series |
| ISO 14213-1998 | 航空航天 飞机结构用扭力管设计的超轻负荷密封精密单列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, rigid, precision, sealed, torque tube design, extra light duty - Inch series |
| ISO 14214-1998 | 航空航天 飞机结构用重负荷密封双列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, double-row, rigid, sealed, heavy duty - Inch series |
| ISO 14215-1998 | 航空航天 飞机结构用重负荷密封精密双列刚性球轴承 英制系列 | Aerospace - Airframe ball bearings, double-row, rigid, precision, sealed, heavy duty - Inch series |
| ISO 14216-1998 | 航空航天 飞机结构用重负荷密封双列自调心球轴承 英制系列 | Aerospace - Airframe ball bearings, double-row, self-aligning, sealed, heavy duty - Inch series |
| ISO 14217-1998 | 航空航天 飞机结构用重负荷密封精密双列自调心球轴承 英制系列 | Aerospace - Airframe ball bearings, double-row, self-aligning, precision, sealed, heavy duty - Inch series |
| ISO 14218-1998 | 航空航天 飞机结构用重负荷密封单列自调心球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, self-aligning, sealed, heavy duty - Inch series |
| ISO 14219-1998 | 航空航天 飞机结构用重负荷密封精密单列自调心球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, self-aligning, precision, sealed, heavy duty - Inch series |
| ISO 14220-1998 | 航空航天 飞机结构用轻负荷密封单列自调心球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, self-aligning, sealed, light duty - Inch series |
| ISO 14221-1998 | 航空航天 飞机结构用轻负荷密封精密单列自调心球轴承 英制系列 | Aerospace - Airframe ball bearings, single-row, self-aligning, precision, sealed, light duty - Inch series |
| ISO 14275-2002 | 航空航天.有条纹的内偏距十字交叉驱动器.米制系列 | Aerospace - Drives, internal, offset cruciform, ribbed - Metric series |
| ISO 14276-2002 | 航空航天.内偏距十字交叉驱动器.米制系列 | Aerospace - Drives, internal, offset cruciform - Metric series |
| ISO 14277-2002 | 航空航天.有条纹的内调整偏差十字形驱动器或无条纹驱动器.米制系列 | Aerospace - Drivers, ribbed, for internal offset cruciform ribbed or unribbed drives - Metric series |
| ISO 14278-2002 | 航空航天.有条纹的内调整偏差十字形精确计量仪或无条纹驱动器.米制系列 | Aerospace - Gauges, for internal offset cruciform ribbed or unribbed drives - Metric series |
| ISO 14279-2002 | 航空航天.内十字形驱动器.米制系列 | Aerospace - Drives, internal, cruciform - Metric series |
| ISO 14280-2002 | 航空航天.有条纹,内十字形驱动器或无条纹驱动器.米制系列 | Aerospace - Drivers, ribbed for internal cruciform ribbed or unribbed drives - Metric series |
| ISO 14281-2002 | 航空航天.有条纹的内十字形精确计量仪或无条纹驱动器.米制系列 | Aerospace - Gauges for internal cruciform ribbed or unribbed drives - Metric series |
| ISO 14300-1-2001 | 航天系统 程序管理 第1部分：程序结构 | Space systems - Programme management - Part 1: Structuring of a programme |
| ISO 14300-2-2002 | 航天系统.程序管理.第2部分:产品保证程序 | Space systems - Programme management - Part 2: Product assurance |
| ISO 14302-2002 | 航天系统.电磁兼容性要求 | Space systems - Electromagnetic compatibility requirements |
| ISO 14303-2002 | 航天系统.运载火箭与航天器的接口 | Space systems - Launch-vehicle-to-spacecraft interfaces |
| ISO 14619-2003 | 航天系统.空间实验.一般要求 | Space systems - Space experiments - General requirements |
| ISO 14620-1-2002 | 航天系统.安全要求.第1部分:系统安全 | Space systems - Safety requirements - Part 1: System safety |
| ISO 14620-2-2000 | 航天系统 安全要求 第2部分:发射现场操作 | Space systems-- Safety requirments - Part 2: Launch site operations |
| ISO 14620-3-2005 | 航天系统.安全要求 第3部分:飞行安全系统 | Space systems - Safety requirements - Part 3: Flight safety systems |
| ISO 14621-1-2003 | 航天系统.电气、电子和电气机械(EEE)零件.第1部分:零件管理 | Space systems - Electrical, electronic and electromechanical (EEE) parts - Part 1: Parts management |
| ISO 14621-2-2003 | 航天系统.电气、电子和机电元件.第2部分:控制程序要求 | Space systems - Electrical, electronic and electromechanical (EEE) parts - Part 2: Control programme requirements |
| ISO 14622-2000 | 航天系统 结构设计 载荷及其诱导环境 | Space systems - Structural design - Loads and induced environment |
| ISO 14623-2003 | 航天系统.压力容器及承压结构.设计与操作 | Space systems - Pressure vessels and pressurized structures - Design and operation |
| ISO 14624-1-2003 | 航天系统.材料的安全和兼容性.第1部分:材料向上易燃性的测定 | Space systems - Safety and compatibility of materials - Part 1: Determination of upward flammability of materials |
| ISO 14624-2-2003 | 航天系统.材料的安全和兼容性.第2部分:电线绝缘和附属材料易燃性的测定 | Space systems - Safety and compatibility of materials - Part 2: Determination of flammability of electrical-wire insulation and accessory materials |
| ISO 14624-3-2005 | 航天系统.材料的安全性和兼容性.第3部分:材料和附属物品产生的废气物测定 | Space systems - Safety and compatibility of materials - Part 3: Determination of offgassed products from materials and assembled articles |
| ISO 14624-4-2003 | 航天系统.材料的安全和兼容性.第4部分:加压气态氧或富氧环境下材料向上易燃性的测定 | Space systems - Safety and compatibility of materials - Part 4: Determination of upward flammability of materials in pressurized gaseous oxygen or oxygen-enriched environments |
| ISO 14624-5-2006 | 航天系统.材料的安全和兼容性.第5部分:航空航天推进器的系统/组件材料的活性测定 | Space systems - Safety and compatibility of materials - Part 5: Determination of reactivity of system/component materials with aerospace propellants |
| ISO 14624-6-2006 | 航天系统.材料的安全和兼容性.第6部分:加工材料与航空航天流反应性测定 | Space systems - Safety and compatibility of materials - Part 6: Determination of reactivity of processing materials with aerospace fluids |
| ISO 14624-7-2006 | 航天系统.材料的安全和兼容性.第7部分:航空航天流体对材料穿透率和渗透性的测定 | Space systems - Safety and compatibility of materials - Part 7: Determination of permeability and penetration of materials to aerospace fluids |
| ISO 1464-1985 | 航空航天 三脚千斤顶 间隙尺寸 | Aerospace; Tripod jacks; Clearance dimensions |
| ISO 14711-2003 | 航天系统.不载人运行的概念产品.定义和使用概念产品指南 | Space systems - Unmanned mission operations concepts - Guidelines for defining and accessing concept products |
| ISO 14721-2003 | 航天数据和信息传输系统.开放式档案信息系统.参考模式 | Space data and information transfer systems - Open archival information system - Reference model |
| ISO 14950-2004 | 航天系统.不载人航天器的可操作性 | Space systems - Unmanned spacecraft operability |
| ISO 14951-1-1999 | 航天系统 流体特性 第1部分:氧 | Space systems - Fluid characteristics - Part 1: Oxygen |
| ISO 14951-10-1999 | 航天系统.流体特性.第10部分:水 | Space systems - Fluid characteristics - Part 10: Water |
| ISO 14951-11-1999 | 航天系统 流体特性 第11部分:氨 | Space systems - Fluid characteristics - Part 11: Ammonia |
| ISO 14951-12-1999 | 航天系统 流体特性 第12部分:二氧化碳 | Space systems - Fluid characteristics - Part 12: Carbon dioxide |
| ISO 14951-13-1999 | 航天系统 流体特性 第13部分:供气用空气 | Space systems - Fluid characteristics - Part 13: Breathing air |
| ISO 14951-2-1999 | 航天系统 流体特性 第2部分:氢推进剂 | Space systems - Fluid characteristics - Part 2: Hydrogen propellant |
| ISO 14951-3 Technical Corrigendum 1-2000 | 航天系统 流体特性 第3部分:氮 技术勘误1 | Space systems - Fluid characteristics - Part 3: Nitrogen; Technical Corrigendum 1 |
| ISO 14951-3-1999 | 航天系统 流体特性 第3部分:氮 | Space systems - Fluid characteristics - Part 3: Nitrogen |
| ISO 14951-4 Technical Corrigendum 1-2000 | 航天系统 流体特性 第4部分:氦 技术勘误1 | Space systems - Fluid characteristics - Part 4: Helium; Technical Corrigendum 1 |
| ISO 14951-4-1999 | 航天系统 流体特性 第4部分:氦 | Space systems - Fluid characteristics - Part 4: Helium |
| ISO 14951-5 Technical Corrigendum 1-2004 | 航天系统.流体特性.第5部分:四氧化二氮推进剂.技术勘误1 | Space systems - Fluid characteristics - Part 5: Nitrogen tetroxide propellant; Technical Corrigendum 1 |
| ISO 14951-5-1999 | 航天系统 流体特性 第5部分:四氧化二氮推进剂 | Space systems - Fluid characteristics - Part 5: Nitrogen tetroxide propellant |
| ISO 14951-6 Technical Corrigendum 1-2004 | 航天系统.流体特性.第6部分:一甲基肼推进剂.技术勘误1 | Space systems - Fluid characteristics - Part 6: Monomethylhydrazine propellant; Technical Corrigendum 1 |
| ISO 14951-6-1999 | 航天系统 流体特性 第6部分:一甲基肼推进剂 | Space systems - Fluid characteristics - Part 6: Monomethylhydrazine propellant |
| ISO 14951-7 Technical Corrigendum 1-2004 | 航天系统.流体特性.第7部分:肼推进剂.技术勘误1 | Space systems - Fluid characteristics - Part 7: Hydrazine propellant; Technical Corrigendum 1 |
| ISO 14951-7-1999 | 航天系统 流体特性 第7部分:肼推进剂 | Space systems - Fluid characteristics - Part 7: Hydrazine propellant |
| ISO 14951-8-1999 | 航天系统 流体特性 第8部分:煤油推进剂 | Space systems - Fluid characteristics - Part 8: Kerosene propellant |
| ISO 14951-9 Technical Corrigendum 1-2000 | 航天系统 流体特性 第9部分:氩 技术勘误1 | Space systems - Fluid characteristics - Part 9: Argon; Technical Corrigendum 1 |
| ISO 14951-9-1999 | 航天系统 流体特性 第9部分:氩 | Space systems - Fluid characteristics - Part 9: Argon |
| ISO 14952-1-2003 | 航天系统.流体系统的表面清洁度.第1部分:词汇 | Space systems - Surface cleanliness of fluid systems - Part 1: Vocabulary |
| ISO 14952-2-2003 | 航天系统.流体系统的表面清洁度.第2部分:清洁度等级 | Space systems - Surface cleanliness of fluid systems - Part 2: Cleanliness levels |
| ISO 14952-3-2003 | 航天系统.流体系统的表面清洁度.第3部分:非挥发性残余物和粒子浓度的测定用分析方法 | Space systems - Surface cleanliness of fluid systems - Part 3: Analytical procedures for the determination of nonvolatile residues and particulate contamination |
| ISO 14952-4-2003 | 航天系统.流体系统的表面清洁度.第4部分:初步清洁过程 | Space systems - Surface cleanliness of fluid systems - Part 4: Rough-cleaning processes |
| ISO 14952-5-2003 | 航天系统.流体系统的表面清洁度.第5部分:干燥过程 | Space systems - Surface cleanliness of fluid systems - Part 5: Drying processes |
| ISO 14952-6-2003 | 航天系统.流体系统的表面清洁度.第6部分:精细清洁过程 | Space systems - Surface cleanliness of fluid systems - Part 6: Precision-cleaning processes |
| ISO 14953-2000 | 航天系统 结构设计 运载器的静态鉴定试验载荷量级的确定 | Space systems - Structural design - Determination of loading levels for static qualification testing of launch vehicles |
| ISO 15387-2005 | 航天系统.单结太阳能电池.测量和校准规程 | Space systems - Single-junction solar cells - Measurements and calibration procedures |
| ISO 15389 AMD 1-2005 | 航天系统.空中到地面的临时管缆.修改件1:防止意外的交叉接合 | Space systems - Flight-to-ground umbilicals; Amendment 1: Prevention of accidental cross-connection |
| ISO 15389 Technical Corrigendum 1-2006 | 航天系统.空中到地面的临时管缆.技术勘误1 | Space systems - Flight-to-ground umbilicals; Technical Corrigendum 1 |
| ISO 15390-2004 | 航天环境(天然的和人工的).银河宇宙射线模型 | Space environment (natural and artificial) - Galactic cosmic ray model |
| ISO 1540-2006 | 航空航天.飞行器电气系统的特性 | Aerospace - Characteristics of aircraft electrical systems |
| ISO 15859-1-2004 | 航天系统.流动特性、取样和试验方法.第1部分:氧 | Space systems - Fluid characteristics, sampling and test methods - Part 1: Oxygen |
| ISO 15859-10-2004 | 航天系统.流动特性、取样和试验方法.第10部分:水 | Space systems - Fluid characteristics, sampling and test methods - Part 10: Water |
| ISO 15859-11-2004 | 航天系统.流动特性、取样和试验方法.第11部分:氨 | Space systems - Fluid characteristics, sampling and test methods - Part 11: Ammonia |
| ISO 15859-12-2004 | 航天系统.流动特性、取样和试验方法.第12部分:二氧化碳 | Space systems - Fluid characteristics, sampling and test methods - Part 12: Carbon dioxide |
| ISO 15859-13-2004 | 航天系统.流动特性、取样和试验方法.第13部分:呼吸用空气 | Space systems - Fluid characteristics, sampling and test methods - Part 13: Breathing air |
| ISO 15859-2-2004 | 航天系统.流动特性、取样和试验方法.第2部分:氢 | Space systems - Fluid characteristics, sampling and test methods - Part 2: Hydrogen |
| ISO 15859-3-2004 | 航天系统.流动特性、取样和试验方法.第3部分:氮 | Space systems - Fluid characteristics, sampling and test methods - Part 3: Nitrogen |
| ISO 15859-4-2004 | 航天系统.流动特性、取样和试验方法.第4部分:氦 | Space systems - Fluid characteristics, sampling and test methods - Part 4: Helium |
| ISO 15859-5-2004 | 航天系统.流动特性、取样和试验方法.第5部分:四氧化氮推进剂 | Space systems - Fluid characteristics, sampling and test methods - Part 5: Nitrogen tetroxide propellants |
| ISO 15859-6-2004 | 航天系统.流动特性、取样和试验方法.第6部分:一甲基肼推进剂 | Space systems - Fluid characteristics, sampling and test methods - Part 6: Monomethylhydrazine propellant |
| ISO 15859-7-2004 | 航天系统.流动特性、取样和试验方法.第7部分:肼推进剂 | Space systems - Fluid characteristics, sampling and test methods - Part 7: Hydrazine propellant |
| ISO 15859-8-2004 | 航天系统.流动特性、取样和试验方法.第8部分:煤油推进剂 | Space systems - Fluid characteristics, sampling and test methods - Part 8: Kerosine propellant |
| ISO 15859-9-2004 | 航天系统.流动特性、取样和试验方法.第9部分:氩 | Space systems - Fluid characteristics, sampling and test methods - Part 9: Argon |
| ISO 15860-2006 | 航天系统.气体污染.现场试验测量方法 | Space systems - Gas contamination - Measurement methods for field tests |
| ISO 15863-2003 | 航天系统.航天飞机与运载工具间接口的控制文献 | Space systems - Spacecraft-to-launch-vehicle interface control document |
| ISO 15865-2005 | 航天系统.合格评定 | Space systems - Qualification assessment |
| ISO 15872-2002 | 航空航天.UNJ螺纹.测量 | Aerospace - UNJ threads - Gauging |
| ISO 15889-2003 | 航天数据和信息传送系统.数据描述语言.EAST规范 | Space data and information transfer systems - Data description language - EAST specification |
| ISO 16031-1-2002 | 航空航天液压系统.英制系列O型密封圈:内直径和横截面,公差和尺寸认证编码.第1部分:液压系统近似公差 | Aerospace fluid systems - O-rings, inch series: Inside diameters and cross sections, tolerances and size-identification codes - Part 1: Close tolerances for hydraulic systems |
| ISO 16031-2-2003 | 航空航天流体系统.英制系列O型密封圈:内直径和横截面、公差和尺寸识别码.第2部分:非液压系统的标准公差 | Aerospace fluid systems - O-rings, inch series: Inside diameters and cross-sections, tolerances and size-identification codes - Part 2: Standard tolerances for non-hydraulic systems |
| ISO 16091-2002 | 航天系统.统一的后勤支援 | Space systems - Integrated logistic support |
| ISO 16458-2004 | 航天系统.不载人航天器运输.一般要求 | Space systems - Unmanned spacecraft transportation - General requirements |
| ISO 17057-1999 | 航空航天 实心铆钉 试验方法 | Aerospace - Rivets, solid - Test method |
| ISO 17401-2004 | 航天系统.运载工具用航天飞行器接口要求文献 | Space systems - Spacecraft interface requirements document for launch vehicle services |
| ISO 17666-2003 | 航天系统.风险管理 | Space systems - Risk management |
| ISO 19933-2007 | 航天系统.航天器发射环境试验报告格式 | Space systems - Format for spacecraft launch environment test report |
| ISO 2020-1-1997 | 航空航天 航空器操纵系统用预成形柔性钢丝绳 第1部分:尺寸和负载能力 | Aerospace - Preformed flexible steel wire rope for aircraft controls - Part 1: Dimensions and loads |
| ISO 2020-2-1997 | 航空航天 航空器操纵系统用预成形柔性钢丝绳 第2部分:技术规范 | Aerospace - Preformed flexible steel wire rope for aircraft controls - Part 2: Technical specification |
| ISO 21347-2005 | 航天系统.断裂和损坏控制 | Space systems - Fracture and damage control |
| ISO 21348-2007 | 航天环境(天然的和人造的).太阳辐照度的测定规程 | Space environment (natural and artificial) - Process for determining solar irradiances |
| ISO 21349-2007 | 航天系统.规划评定 | Space systems - Project reviews |
| ISO 21350-2007 | 航天系统.现货供应产品的利用 | Space systems - Off-the-shelf item utilization |
| ISO 21351-2005 | 航天系统.功能和技术规范 | Space systems - Functional and technical specifications |
| ISO 21961-2003 | 航天数据和信息传输系统.数据实体字典规范语言(DEDSL).抽象语句 | Space data and information transfer systems - Data entity dictionary specification language (DEDSL) - Abstract syntax |
| ISO 21962-2003 | 航天数据和信息传输系统.数据实体字典规范语言(DEDSL).PVL语法 | Space data and information transfer systems - Data entity dictionary specification language (DEDSL) - PVL syntax |
| ISO 22072-2005 | 航空航天.电动流体静力传动装置(EHA).采购规范中定义的特性 | Aerospace - Electrohydrostatic actuator (EHA) - Characteristics to be defined in procurement specifications |
| ISO 22538-1-2007 | 航天系统.氧气安全.第1部分:氧气系统及组件的设计 | Space systems - Oxygen safety - Part 1: Design of oxygen systems and components |
| ISO 22538-2-2007 | 航天系统.氧气安全.第2部分:氧气系统及组件用金属材料的选择 | Space systems - Oxygen safety - Part 2: Selection of metallic materials for oxygen systems and components |
| ISO 22538-3-2007 | 航天系统.氧气安全.第3部分:氧气系统及组件用非金属材料的选择 | Space systems - Oxygen safety - Part 3: Selection of non-metallic materials for oxygen systems and components |
| ISO 22538-4-2007 | 航天系统.氧气安全.第4部分:氧气系统及组件的危险分析 | Space systems - Oxygen safety - Part 4: Hazards analyses for oxygen systems and components |
| ISO 22641-2005 | 航天数据和信息传送系统.TM(遥测技术)同步和信道编码 | Space data and information transfer systems - TM (telemetry) synchronization and channel coding |
| ISO 22642 Technical Corrigendum 1-2007 | 航天数据和信息传输系统.TC(遥测指令)同步和信道编码.技术勘误1 | Space data and information transfer systems - TC (telecommand) synchronization and channel coding; Technical Corrigendum 1 |
| ISO 22642-2005 | 航天数据和信息传送系统.TC(遥测指令)同步和信道编码 | Space data and information transfer systems - TC (telecommand) synchronization and channel coding |
| ISO 22643-2003 | 航天数据和信息传送系统.数据实体字典规范语言(DEDSL).XML/DTD语句 | Space data and information transfer systems - Data entity dictionary specification language (DEDSL) - XML/DTD Syntax |
| ISO 22644-2006 | 航天数据和信息传送系统.轨道数据文电 | Space data and information transfer systems - Orbit data messages |
| ISO 22645-2005 | 航天数据和信息传送系统.TM(遥测技术)航天数据链接协议 | Space data and information transfer systems - TM (telemetry) space data link protocol |
| ISO 22646-2005 | 航天数据和信息传送系统.航天数据包协议 | Space data and information transfer systems - Space packet protocol |
| ISO 22647-2006 | 航天数据和信息传输系统.空间链路识别符 | Space data and information transfer systems - Space link identifiers |
| ISO 22663-2007 | 航天数据和信息传输系统.接近1的空间链接协议.数据链路层 | Space data and information transfer systems - Proximity-1 space link protocol - Data link layer |
| ISO 22664-2005 | 航天数据和信息传送系统.TC(遥测指令)航天数据链接协议 | Space data and information transfer systems - TC (telecommand) space data link protocol |
| ISO 22666-2007 | 航天数据和信息传输系统.AOS(高级轨道系统)航天数据连接协议 | Space data and information transfer systems - AOS (advanced orbiting systems) space data link protocol |
| ISO 22667-2005 | 航天数据和信息传送系统.通信操作过程-1 | Space data and information transfer systems - Communication operations Procedure-1 |
| ISO 22671-2007 | 航天数据和信息传送系统.空间链路扩展(SLE).向前通信链路传送装置(CLTU)业务 | Space data and information transfer systems - Space link extension (SLE) - Forward communications link transmission unit (CLTU) service |
| ISO 22672-2006 | 航天数据和信息传输系统.空间链路扩展(SLE).正向空间数据包业务 | Space data and information transfer systems - Space link extension (SLE) - Forward space packet service |
| ISO 23038-2006 | 航天系统.航天用太阳能电池.电子和质子辐射试验法 | Space systems - Space solar cells - Electron and proton irradiation test methods |
| ISO 23933-2006 | 航空航天.等级为135 °C/20.684 kPa (275 °F/3.000 psi) 和135 °C/21.000 kPa (275 °F/3.046 psi)的芳族 | Aerospace - Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 °C/20.684 kPa (275 °F/3.000 psi) and 135 °C/21.000 kPa (275 °F/3.046 psi) - Procurement specification |
| ISO 245-1998 | 航空航天 锁紧丝 直径 | Aerospace - Lockwire - Diameters |
| ISO 2635-2003 | 航空器.一般用途的飞机电缆和航空航天应用的导线.尺寸和特性 | Aircraft - Conductors for general purpose aircraft electrical cables and aerospace applications - Dimensions and characteristics |
| ISO 2964-1985 | 航空航天 管材 外径和管壁厚度 米制尺寸 | Aerospace; Tubing; Outside diameters and thicknesses; Metric dimensions |
| ISO 3161-1999 | 航空航天 UNJ螺纹 一般要求和极限尺寸 | Aerospace - UNJ threads - General requirements and limit dimensions |
| ISO 3168-1998 | 航空航天.等级为:1100MPa(环境温度)/235℃、1100MPa(环境温度/315℃和1100MPa(环境温度)/425℃、带有沉孔及 | Aerospace - Nuts, anchor, self-locking, fixed, single lug, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3185-1993 | 航空航天 强度等级小于或等于1100MPa、有涂层或无涂层、金属材料制成、短的或中等长度MJ螺纹、大径杆型的普 | Aerospace; bolts, normal bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa; dimensions |
| ISO 3186-1994 | 航空航天 强度等级1250 MPa～1800 MPa、有涂层或无涂层、金属材料制成的标准柄、短或中等长度MJ螺纹、大径 | Aerospace - Bolts, large bihexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes 1250 MPa to 1800 MPa - Dimensions |
| ISO 3191-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, fixed, single lug, reduced series, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3193 Technical Corrigendum 1-1992 | 航空航天 强度等级小于或等于1100 MPa、有涂层或无涂层、金属材料制成、短的或中等长度MJ螺纹、大径杆型普 | Aerospace; bolts, normal hexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPA; dimensions; technical corrigendum 1 |
| ISO 3193-1991 | 航空航天 强度等级小于或等于1100 MPa、有涂层或无涂层、金属材料制成、短的或中等长度MJ螺纹、大径杆型普 | Aerospace; bolts, normal hexagonal head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa; dimensions |
| ISO 3202-1997 | 航空航天 强度等级小于或等于1100 MPa、有涂层或无涂层、金属材料制成、带内偏高扭矩十字槽或不打滑扳动结 | Aerospace - Screws, pan head, internal offset cruciform ribbed or unribbed drive, threaded to head, MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa - Dimensions |
| ISO 3203-1993 | 航空航天.强度等级小于或等于1100MPa、有涂层或无涂层、金属材料制成的标准直径或中径柄、长MJ螺纹、普通双 | Aerospace; bolts, normal bihexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa; dimensions |
| ISO 3209-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, floating, two lug, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3221-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, fixed, 90° corner, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3222-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, fixed, closed corner, reduced series, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3223-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, fixed, two lug, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3224-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, floating, single lug, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3225-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, fixed, two lug, reduced series, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 3230-1998 | 航空航天.金属制有或无表面处理的带圆墩坑的正常100°沉头实心铆钉.尺寸 | Aerospace - Rivets, solid, 100 ° normal countersunk head with dome, metallic material, with or without surface treatment - Dimensions |
| ISO 3353-1-2002 | 航空航天.引导和收尾螺纹.第1部分:滚压外螺纹 | Aerospace - Lead and runout threads - Part 1: Rolled external threads |
| ISO 3353-2-2002 | 航空航天.引导和收尾螺纹.第2部分:内螺纹 | Aerospace - Lead and runout threads - Part 2: Internal threads |
| ISO 4095-1998 | 航空航天 十二角传动 扳手结构 米制系列 | Aerospace - Bihexagonal drives - Wrenching configuration - Metric series |
| ISO 4147-1997 | 航空航天.等级为:600 MPa(环境温度)/120℃、600 MPa(环境温度)/235℃、900 MPa(环境温度)/425℃、1100 MPa( | Aerospace - Nuts, hexagonal, slotted (castellated), normal height, normal across flats, with MJ threads, classifications: 600 MPa (at ambient temperature)/120 °C, 600 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/425 °C, 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C, 1100 MPa (at ambient temperature)/650 °C, 1210 MPa (at ambient temperature)/730 ° C, 1250 MPa (at ambient temperature)/235 ° C and 1550 MPa (at ambient temperature)/ 600° C - Dimensions |
| ISO 44-1975 | 航空航天 手柄操纵的双位(开/关)开关 操作方向 | Aerospace; Lever-operated, two-position, ON/OFF switches; Directions of operation |
| ISO 5843-1-1985 | 航空航天器结构 同义术语表 第1部分:航空航天电气设备 三种语言版 | Aerospace construction; List of equivalent terms; Part 1 : Aerospace electrical equipment Trilingual edition |
| ISO 5843-10-1988 | 航空航天 同义术语表 第10部分:飞机结构 三种语言版 | Aerospace; list of equivalent terms; part 10: aircraft structure |
| ISO 5843-2-1990 | 航空航天 同义术语表 第2部分:航空航天用铆钉 三种语言版 | Aerospace; list of equivalent terms; part 2: aerospace rivets |
| ISO 5843-3-1997 | 航空航天 同义术语表 第3部分:航空航天用螺栓和螺母 三种语言版 | Aerospace - List of equivalent terms - Part 3: Aerospace bolts and nuts |
| ISO 5843-4-1990 | 航空航天 同义术语表 第4部分:飞行力学 三种语言版 | Aerospace; list of equivalent terms; part 4: flight dynamics |
| ISO 5843-5-1990 | 航空航天 同义术语表 第5部分:航空器设备的环境条件和工作条件 三种语言版 | Aerospace; list of equivalent terms; part 5; environmental and operating conditions for aircraft equipment |
| ISO 5843-6-1985 | 航空航天 同义术语表 第6部分:标准大气 三种语言版 | Aerospace; List of equivalent terms; Part 6 : Standard atmosphere Trilingual edition |
| ISO 5843-8-1988 | 航空航天 同义术语表 第8部分:航空器可靠性 三种语言版 | Aerospace; list of equivalent terms; part 8: aircraft reliability |
| ISO 5843-9-1988 | 航空航天 同义术语表 第9部分:航空器 三种语言版 | Aerospace; list of equivalent terms; part 9: aircraft |
| ISO 5855-1-1999 | 航空航天 MJ螺纹 第1部分:一般要求 | Aerospace - MJ threads - Part 1: General requirements |
| ISO 5855-2-1999 | 航空航天 MJ螺纹 第2部分:螺栓和螺母螺纹的极限尺寸 | Aerospace - MJ threads - Part 2: Limit dimensions for bolts and nuts |
| ISO 5855-3-1999 | 航空航天 MJ螺纹 第3部分:液体系统管接头螺纹系统的极限尺寸 | Aerospace - MJ threads - Part 3: Limit dimensions for fittings for fluid systems |
| ISO 5856-1991 | 航空航天 强度等级小于或等于1100 MPa、金属材料制成、有涂层或无涂层、带有中或短长度MJ螺纹、大径杆型及 | Aerospace; screws, 100 normal countersunk head, internal offset cruciform ribbed drive, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa; dimensions |
| ISO 5857-1988 | 航空航天 强度等级1250 MPa带有MJ螺纹的合金钢凸头螺栓 采购规范 | Aerospace; alloy steel protruding head bolts with strength classification 1250 MPa and MJ threads; procurement specification |
| ISO 5858-1999 | 航空航天.最高工作温度小于或等于425℃的自锁螺母.采购规范 | Aerospace - Nuts, self-locking, with maximum operating temperature less than or equal to 425 °C - Procurement specification |
| ISO 5859-1991 | 航空航天 液压气动系统和组件原理图用图形符号 | Aerospace; graphic symbols for schematic drawings of hydraulic and pneumatic systems and components |
| ISO 5878 ADD 1-1983 | 航空航天用参考大气 补充1 | Addendum 1-1983 |
| ISO 5878 ADD 2-1983 | 航空航天用参考大气 补充2 | Reference atmospheres for aerospace use; addendum 2 |
| ISO 5878 AMD 1-1990 | 航空航天用参考大气 修改1 | Reference atmospheres for aerospace use; amendment 1 |
| ISO 5878-1982 | 航空航天用参考大气 | Reference atmospheres for aerospace use |
| ISO 5884-1987 | 航空航天 流体系统和组件 液压油液固体颗粒污染的系统取样和测量方法 | Aerospace; Fluid systems and components; Methods for system sampling and measuring the solid particle contamination of hydraulic fluids |
| ISO 6771-2007 | 航空航天.流体系统和部件.压力和温度分类 | Aerospace - Fluid systems and components - Pressure and temperature classifications |
| ISO 6772-1988 | 航空航天 流体系统 液压软管、导管和接头组件的冲击试验 | Aerospace; fluid systems; impulse testing of hydraulic hose, tubing and fitting assemblies |
| ISO 6773-1994 | 航空航天 流体系统 管道及配件的热冲击试验 | Aerospace - Fluid systems - Thermal shock testing of piping and fittings |
| ISO 7169-2007 | 航空航天.液压系统用24°锥形的、压力范围截至3000psi或21000kPa的可拆卸管接头.采购规范(英制/米制) | Aerospace - Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3000 psi or 21000 kPa - Procurement specification, inch/metric |
| ISO 7258-1984 | 航空航天用聚四氟乙烯(PTFE)管材 密度和相对密度的测定方法 | Polytetrafluoroethylene (PTFE) tubing for aerospace applications; Methods for the determination of the density and relative density |
| ISO 7314-2002 | 航空航天.液压系统.金属软管组件 | Aerospace - Fluid systems - Metal hose assemblies |
| ISO 7315-1988 | 航空航天 液压系统安装用“P”形卡箍(环状卡箍) 包容尺寸 | Aerospace; "P" clamps (loop clamps) for fluid systems; envelope dimensions |
| ISO 7319-1992 | 航空航天.流体系统.24°锥孔米制管接头的接口 | Aerospace; fluid systems; interface of 24° cone metric couplings |
| ISO 7320-1992 | 航空航天 流体系统螺纹密封连接接头 尺寸 | Aerospace; couplings, threaded and sealed, for fluid systems; dimensions |
| ISO 7332-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 7403-1998 | 航空航天 花键传动 扳手结构 米制系列 | Aerospace - Spline drives - Wrenching configuration - Metric series |
| ISO 7481-2000 | 航空航天 最高工作温度小于或等于425℃的自锁螺母 试验方法 | Aerospace - Nuts, self-locking, with maximum operating temperature less than or equal to 425 °C - Test methods |
| ISO 7661-1984 | 航空航天 流体系统 可轴向调准的管路安装用夹块 设计标准和合格鉴定试验 米制系列 | Aerospace; Fluid systems; Clamp blocks for tube lines having axial alignment; Design standard and qualification testing; Metric series |
| ISO 7689-1988 | 航空航天 强度等级1100 MPa、带MJ螺纹的合金钢螺栓 采购规范 | Aerospace; alloy steel bolts with strength classification 1100 MPa and MJ threads; procurement specification |
| ISO 7913-1994 | 航空航天 米制螺栓和螺钉的形状和位置公差 | Aerospace - Bolts and screws, metric - Tolerances of form and position |
| ISO 7961-1994 | 航空航天 螺栓 试验方法 | Aerospace; bolts; test methods |
| ISO 7995-2002 | 航空航天.涂覆或未涂覆自锁式六角形MJ螺纹螺母.等级:1100MPa/235℃、1100MPa/315℃ 或1100MPa/425℃.尺寸 | Aerospace - Nuts, hexagonal, self-locking, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 8074-1985 | 航空航天 奥氏体不锈钢零件的表面处理 | Aerospace; Surface treatment of austenitic stainless steel parts |
| ISO 8075-1985 | 航空航天 可淬硬的不锈钢零件表面处理 | Aerospace; Surface treatment of hardenable stainless steel parts |
| ISO 8078-1984 | 航空航天工艺 铝合金的阳极化处理 无着色涂层的硫酸工艺规程 | Aerospace process; Anodic treatment of aluminium alloys; Sulfuric acid process, undyed coating |
| ISO 8079-1984 | 航空航天工艺 铝合金的阳极化处理 带着色涂层的硫酸工艺规程 | Aerospace process; Anodic treatment of aluminium alloys; Sulfuric acid process, dyed coating |
| ISO 8080-1985 | 航空航天 钛和钛合金的阳极化处理 硫酸工艺规程 | Aerospace; Anodic treatment of titanium and titanium alloys; Sulfuric acid process |
| ISO 8081-1985 | 航空航天工艺 铝合金的化学转化涂镀 一般用途 | Aerospace process; Chemical conversion coating for aluminium alloys; General purpose |
| ISO 8168-1988 | 航空航天 强度等级为1100 MPa、带MJ螺纹的耐腐蚀和耐热钢制螺栓 采购规范 | Aerospace; corrosion- and heat-resisting steel bolts with strength classification 1100 MPa and MJ threads; procurement specification |
| ISO 8177-1986 | 航空航天 流体系统用“Ω”形卡箍(鞍型卡箍) 尺寸 | Aerospace; Omega clamps (saddle clamps) for fluid systems; Dimensions |
| ISO 8278-1986 | 航空航天 液压式压力补偿变流量泵 一般要求 | Aerospace; Hydraulic, pressure compensated, variable delivery pumps; General requirements |
| ISO 8279-1997 | 航空航天.等级为:600 MPa(环境温度)/120℃、600 MPa(环境温度)/235℃、900 MPa(环境温度)/425℃、1100MPa( | Aerospace - Nuts, hexagonal, plain, normal height, normal across flats, with MJ threads, classifications: 600 MPa (at ambient temperature)/120 °C, 600 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/425 °C, 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C, 1100 MPa (at ambient temperature)/650 °C, 1210 MPa (at ambient temperature)/730 ° C, 1250 MPa (at ambient temperature)/235 ° C and 1550 MPa (at ambient temperature)/ 600° C - Dimensions |
| ISO 8280-1993 | 航空航天 由金属材料制成,经过或没有经过表面处理的普通头实心铆钉 尺寸 | Aerospace; rivets, solid, universal head, metallic material, with or without surface treatment; dimensions |
| ISO 8399-1-1998 | 航空航天 附件驱动和安装法兰(米制系列) 第1部分:设计准则 | Aerospace - Accessory drives and mounting flanges (Metric series) - Part 1: Design criteria |
| ISO 8399-2-1998 | 航空航天 附件驱动和安装法兰(米制系列) 第2部分:尺寸 | Aerospace - Accessory drives and mounting flanges (Metric series) - Part 2: Dimensions |
| ISO 8479-1986 | 航空航天 流体系统的“Q”形卡箍 尺寸 | Aerospace; "Q" clamps (centre-mounted clamps) for fluid systems; Dimensions |
| ISO 8538-1999 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃、带沉孔 | Aerospace - Nuts, hexagonal, self-locking, with counterbore and captive washer, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 8574-2004 | 航空航天.液压系统管路安装.弯管的合格试验 | Aerospace - Hydraulic system tubing - Qualification tests for bent tubes |
| ISO 8575-1990 | 航空航天 流体系统 液压系统管路安装 | Aerospace; fluid systems; hydraulic system tubing |
| ISO 8591-1-1989 | 航空航天 锻铝和铝合金 检验、试验和供货要求 第1部分:一般要求 | Aerospace; wrought aluminium and aluminium alloys; inspection, testing and supply requirements; part 1: general requirements |
| ISO 8625-1-1993 | 航空航天 流体系统 词汇 第1部分:与压力有关的通用术语和定义 两种语言版 | Aerospace; fluid systems; vocabulary; part 1: general terms and definitions relating to pressure |
| ISO 8625-2-1991 | 航空航天 流体系统 词汇 第2部分:与流动有关的通用术语和定义 两种语言版 | Aerospace; fluid systems; vocabulary; part 2: general terms and definitions relating to flow |
| ISO 8625-3-1991 | 航空航天 流体系统 词汇 第3部分:与温度有关的通用术语和定义 两种语言版 | Aerospace; fluid systems; vocabulary; part 3: general terms and definitions relating to temperature |
| ISO 8641-1987 | 航空航天 最高工作温度高于425℃的自锁螺母 采购规范 | Aerospace; Self-locking nuts with maximum operating temperature greater than 425 degrees C; Procurement specification |
| ISO 8642-1986 | 航空航天 最高工作温度高于425℃的自锁螺母 试验方法 | Aerospace; Self-locking nuts with maximum operating temperature greater than 425 degrees C; Test methods |
| ISO 8775-1988 | 航空航天 流体系统用气氧充填接头(新型) 尺寸(英制) | Aerospace; gaseous oxygen replenishment connection for use in fluid systems (new type); dimensions (inch series) |
| ISO 8788-2000 | 航空航天 米制螺母 形状和位置公差 | Aerospace - Nuts, metric - Tolerances of form and position |
| ISO 8913-2006 | 航空航天.轻型聚四氟乙烯(PTFE)软管组件.等级：400℉/3000psi(204℃/20684kPa)和204℃/21000 kPa(400℉/304 | Aerospace - Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 °F/3 000 psi (204 °C/20 684 kPa) and 204 °C/21 000 kPa (400 °F/3 046 psi) - Procurement specification |
| ISO 8940-2002 | 航空航天.锚式自锁密封自定位双耳沉孔螺母.级别:900MPa/120℃,900MPa/175℃,C级和900MPa/235℃.尺寸 | Aerospace - Nuts, anchor, self-locking, sealing, floating, two-lug, with counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/120 °C, 900 MPa (at ambient temperature)/175 °C and 900 MPa (at ambient temperature)/235 °C - Dimensions |
| ISO 9139-1998 | 航空航天 普通或开槽螺母 采购规范 | Aerospace - Nuts, plain or slotted (castellated) - Procurement specification |
| ISO 9140-1998 | 航空航天 普通或开槽螺母 试验方法 | Aerospace - Nuts, plain or slotted (castellated) - Test methods |
| ISO 9152-1998 | 航空航天 强度等级为1100 MPa的钛合金MJ螺纹螺栓 采购规范 | Aerospace - Bolts, with MJ threads, in titanium alloys, strength class 1100 MPa - Procurement specification |
| ISO 9154-1999 | 航空航天 由强度等级为1550 MPa的耐热镍基合金制成的带MJ螺纹的螺栓 采购规范 | Aerospace - Bolts, with MJ threads, made of heat-resistant nickel-based alloy, strength class 1550 MPa - Procurement specification |
| ISO 9156-1998 | 航空航天.等级为:1100 MPa(环境温度)/235℃、1100 MPa(环境温度)/315℃和1100 MPa(环境温度)/425℃,带沉孔 | Aerospace - Nuts, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, with MJ threads, classifications: 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/315 °C and 1100 MPa (at ambient temperature)/425 °C - Dimensions |
| ISO 9157-2002 | 航空航天.等级为:1100MPa(室温下)/425℃、1100MPa(室温下)/650℃、1210MPa(室温下)/425℃、1210MPa(室温下) | Aerospace - Nuts, spline-drive, self-locking, with MJ threads, classifications: 1100 MPa (at ambient temperature)/425°C, 1100 MPa (at ambient temperature)/650°C, 1210 MPa (at ambient temperature)/425°C, 1210 MPa (at ambient temperature)/730°C, 1550 MPa (at ambient temperature)/235°C, 1550 MPa (at ambient temperature)/425°C and 1550 MPa (at ambient temperature)/600°C - Dimensions |
| ISO 9199-1998 | 航空航天.等级为:1100 MPa(环境温度)/425℃、1100 MPa(环境温度)/650℃、1210 MPa(环境温度)/425℃、1210 M | Aerospace - Nuts, bihexagonal, self-locking, MJ threads, classifications: 1100 MPa (at ambient temperature)/425 °C, 1100 MPa (at ambient temperature)/650 °C, 1210 MPa (at ambient temperature)/425 °C, 1210 MPa (at ambient temperature)/730 °C, 1550 MPa (at ambient temperature)/235 °C, 1550 MPa (at ambient temperature)/425 °C and 1550 MPa (at ambient temperature)/ 600 °C - Dimensions |
| ISO 9206-1990 | 航空航天 恒流量液压马达 一般规范 | Aerospace; constant displacement hydraulic motors; general specifications |
| ISO 9216-2002 | 航空航天.滑轮用合金钢和镀镉或耐腐蚀钢和钝化六角带槽(齿形头)螺母.尺寸和质量 | Aerospace - Nuts, hexagonal, slotted (castellated), for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivated - Dimensions and masses |
| ISO 9217-2002 | 航空航天.滑轮用合金钢和镀镉或耐腐蚀钢和钝化带埋头孔的倒角垫圈.尺寸和质量 | Aerospace - Washers, chamfered, with counterbore, for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivated - Dimensions and masses |
| ISO 9218-2002 | 航空航天.滑轮用合金钢和镀镉或耐腐蚀钢和钝化平垫圈.尺寸和质量 | Aerospace - Washers, flat, for pulleys, in alloy steel and cadmium plated or in corrosion-resistant steel and passivated - Dimensions and masses |
| ISO 9219-2002 | 航空航天.滑轮用合金钢和镀镉或钛合金钢、MoS<下标2>润滑或耐腐蚀钢和钝化的紧公差柄、短螺纹薄六角头螺栓. | Aerospace - Bolts, thin hexagonal head, for pulleys, close tolerance shank, short thread, in alloy steel and cadmium-plated or in titanium alloy steel, MoS<(Index)2> lubricated or in corrosion-resistant steel and passivated - Dimensions and masses |
| ISO 9254-1993 | 航空航天.强度等级小于或等于1100MPa、有涂层或无涂层、金属材料制成的标准直径或中径柄、长MJ螺纹、普通在 | Aerospace; bolts, normal spline head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa; dimensions |
| ISO 9255-1993 | 航空航天.强度等级小于或等于1100MPa、有涂层或无涂层、金属材料制成的标准柄、短或中等长度MJ螺纹、普通在 | Aerospace; bolts, normal spline head, normal shank, short or medium length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa; dimensions |
| ISO 9256-1993 | 航空航天.强度等级小于或等于1100MPa、有涂层或无涂层、金属材料制成的标准直径或中径柄、长MJ螺纹、大六角 | Aerospace; bolts, large hexagonal head, normal or pitch diameter shank, long length MJ threads, metallic material, coated or uncoated, strength classes less than or equal to 1100 MPa; dimensions |
| ISO 9418-1998 | 航空航天 铝或铝合金实心铆钉 采购规范 | Aerospace - Rivets, solid, in aluminium or aluminium alloys - Procurement specification |
| ISO 9528-1994 | 航空航天 等级为21000kPa/204℃标准型聚四氟乙烯(PTFE)软管组件 采购规范 | Aerospace - Standard-weight polytetrafluoroethylene (PTFE) hose assemblies, classification 204 C/21 000 kPa - Procurement specification |
| ISO 9538-1996 | 航空航天 液压管路安装接头及管接头 平面弯曲试验 | Aerospace - Hydraulic tubing joints and fittings - Planar flexure test |
| ISO 9609-1996 | 航空航天.等级为:450 MPa(环境温度)/120℃、450 MPa(环境温度)/235℃、600 MPa(环境温度)/425℃、900 MPa( | Aerospace - Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 °C, 450 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/425 °C, 900 MPA (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/315 °C, 900 MPa (at ambient temperature)/650 °C, 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/730 °C and 1250 MPa (at ambient temperature)/600 °C - Dimensions* |
| ISO 9618-1996 | 航空航天.等级为:450 MPa(环境温度)/120℃、450 MPa(环境温度)/235℃、600 MPa(环境温度)/425℃、900 MPa( | Aerospace - Nuts, hexagonal, slotted (castellated), reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature)/120 °C, 450 MPa (at ambient temperature)/235 °C, 600 MPa (at ambient temperature)/425 °C, 900 MPa (at ambient temperature)/235 °C, 900 MPa (at ambient temperature)/315 °C, 900 MPA (at ambient temperature)/ 650 °C, 1100 MPa (at ambient temperature)/235 °C, 1100 MPa (at ambient temperature)/730 °C and 1250 MPa (at ambient temperature)/600 °C - Dimensions |
| ISO 9634-1994 | 航空航天 流体系统 塑料保护罩及管堵的尺寸 | Aerospace - Fluid systems - Dimensions of plastic protective caps and plugs |
| ISO 9679-2006 | 航空航天.流体系统用夹具 | Aerospace - Clamps for fluid systems - Test methods |
| ISO 9736-2000 | 航空航天 航空器操纵钢丝绳的螺纹式钢制有眼端 尺寸及载荷 | Aerospace - Eye-ends, in steel, threaded, for aircraft control wire rope - Dimensions and loads |
| ISO 9737-2000 | 航空航天 航空器操纵钢丝绳用锻制耐腐蚀钢有眼端 尺寸及载荷 | Aerospace - Eye-ends, in corrosion-resistant steel, swaged on aircraft control wire rope - Dimensions and loads |
| ISO 9738-2000 | 航空航天 航空器操纵钢丝绳的旋转套筒 尺寸及载荷 | Aerospace - Turnbarrels, for aircraft control wire rope - Dimensions and loads |
| ISO 9747-2000 | 航空航天 航空器操纵钢丝绳上的锻制耐腐蚀钢双柄球端 尺寸及载荷 | Aerospace - Double-shank ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope - Dimensions and loads |
| ISO 9748-2000 | 航空航天 航空器操纵钢丝绳上的锻制耐腐蚀钢球端 尺寸及载荷 | Aerospace - Ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope - Dimensions and loads |
| ISO 9749-2000 | 航空航天 航空器操纵钢丝绳上的锻制耐腐蚀柱螺栓端 尺寸及载荷 | Aerospace - Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope - Dimensions and loads |
| ISO 9757-2000 | 航空航天 航空器操纵钢丝绳旋转套筒用螺纹式钢制叉形端 尺寸及载荷 | Aerospace - Fork-ends, in steel, threaded, for aircraft control wire rope turnbarrels - Dimensions and loads |
| ISO 9758-2000 | 航空航天 航空器操纵钢丝绳用滚动轴承用螺纹式钢制叉形端 尺寸及载荷 | Aerospace - Fork-ends, in steel, threaded, for rolling bearings, for aircraft control wire rope - Dimensions and loads |
| ISO 9759-2000 | 航空航天 航空器操纵钢丝绳上的锻制耐腐蚀钢叉形端 尺寸及载荷 | Aerospace - Fork-ends, in corrosion-resistant steel, swaged on aircraft control wire rope - Dimensions and loads |
| ISO 9760-2000 | 航空航天 航空器滚动轴承操纵钢丝绳上的锻制耐腐蚀钢制叉形端 尺寸及载荷 | Aerospace - Fork-ends, in corrosion-resistant steel, swaged on aircraft control wire rope, for rolling bearings - Dimensions and loads |
| ISO 9761-2000 | 航空航天 航空器操纵钢丝绳旋转套筒用耐腐蚀钢制锁定夹 尺寸 | Aerospace - Locking clips, in corrosion-resistant steel, for aircraft control wire rope turnbuckles - Dimensions |
| ISO 9762-2000 | 航空航天 航空器操纵钢丝绳组件 尺寸及端部配件组合 | Aerospace - Aircraft control wire rope assemblies - Dimensions and end-fitting combinations |
| ISO 9763-1999 | 航空航天 航空器操纵钢丝绳组件 技术规范 | Aerospace - Aircraft control wire rope assemblies - Technical specification |
| ISO 9938-1994 | 航空航天 强度温度等级为204℃/28000 kPa的聚四氟乙烯软管组件 采购规范 | Aerospace - Polytetrafluoroethylene (PTFE) hose assemblies, classification 204 C/28 000 kPa - Procurement specification |
| ISO 9939-1994 | 航空航天 滑油的压力加油接头(新型) | Aerospace; pressure re-oiling connection (new type) |
| ISO/TR 10201-2001 | 航空航天 电子仪表和系统的标准 | Aerospace - Standards for electronic instruments and systems |
| ISO/TR 12198-1998 | 航空航天 实心铆钉 材料 | Aerospace - Rivets, solid - Materials |
| ISO/TR 17400-2003 | 航天系统.航天全套发射装置、集成站和其他设备.通用测试指南 | Space systems - Space launch complexes, integration sites and other facilities - General testing guidelines |
| ISO/TR 23462-2007 | 航天系统.航天规划管理框架的定义指南 | Space systems - Guidelines to define the management framework for a space project |
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