航天器动力系统标准-分析测试百科网

QJ 2904-1997 固体火箭发动机吊具设计规范

Code for design of solid rocket motor spreader

ICS
CCS: V72
发布: 1997-03-10
实施: 1997-10-01

QJ 2938-1997 固体火箭发动机静止试验质量控制要求

Quality Control Requirements for Static Tests of Solid Rocket Motors

ICS
CCS: V72
发布: 1997-03-10
实施: 1997-10-31

QJ 2140A-1997 弹用涡轮喷气发动机高空模拟试验方法

High-altitude simulation test method for missile turbojet engine

ICS
CCS: V72
发布: 1997-03-08
实施: 1997-10-01

HB 7504.3-1997 飞行模拟器设计和性能的数据要求空气动力和飞行操纵

本标准规定了飞行模拟器的空气动力特性和飞行操纵系统的数据要求。　　本标准适用于民用飞机飞行模拟器，军用模拟器可参照使用。　　本标准为飞行模拟器承制方、使用方、飞机设备的订购方和有关管理机构，提供建造和验证符合空勤人员训练要求的、足够逼真的飞行模拟器所必须的数据范围和内容。　　本标准不是确定飞行模拟器数据要求的唯一方法。

Data requirements for flight simulator design and performance aerodynamics and flight handling

ICS
CCS: V72
发布: 1996-09-13
实施: 1997-10-01

HB 7504.15-1997 飞行模拟器设计和性能的数据要求音响和振动

本标准规定了飞行模拟器音响和振动系统的数据要求。　　本标准适用于民用飞机飞行模拟器，军用模拟器可参照使用。　　本标准为飞行模拟器承制方、使用方、飞机设备的订购方和有关管理机构，提供建造和验证符合空勤人员训练要求的、足够逼真的飞行模拟器所必须的数据范围和内容。　　本标准不是确定飞行模拟器数据要求的唯一方法。

Data Requirements for Flight Simulator Design and Performance Sound and Vibration

ICS
CCS: V72
发布: 1996-09-13
实施: 1997-10-01

HB 7504.5-1997 飞行模拟器设计和性能的数据要求地面操纵特性和起落架系统

本标准规定了飞行模拟器地面操纵特性和起落架系统的数据要求。　　本标准适用于民用飞机飞行模拟器，军用模拟器可参照使用。　　本标准为飞行模拟器承制方、使用方、飞机设备的订购方和有关管理机构，提供建造和验证符合空勤人员训练要求的、足够逼真的飞行模拟器所必须的数据范围和内容。　　本标准不是确定飞行模拟器数据要求的唯一方法。

data requirements for flight simulator design and performance ground handling characteristics and landing gear systems

ICS
CCS: V72
发布: 1996-09-13
实施: 1997-10-01

HB 7504.4-1997 飞行模拟器设计和性能的数据要求飞机重量和惯性矩

本标准规定了飞行模拟器的飞机重量和惯性矩的数据要求。　　本标准适用于民用飞机飞行模拟器，军用模拟器可参照使用。　　本标准为飞行模拟器承制方、使用方、飞机设备的订购方和有关管理机构，提供建造和验证符合空勤人员训练要求的、足够逼真的飞行模拟器所必须的数据范围和内容。　　本标准不是确定飞行模拟器数据要求的唯一方法。

Aircraft weight and moment of inertia data requirements for flight simulator design and performance

ICS
CCS: V72
发布: 1996-09-13
实施: 1997-10-01

HB 7504.6-1997 飞行模拟器设计和性能的数据要求动力装置系统

本标准规定了飞行模拟器所有与动力装置系统有关系统的数据要求。　　本标准适用于民用飞机飞行模拟器，军用模拟器可参照使用。　　本标准为飞行模拟器承制方、使用方、飞机设备的订购方和有关管理机构，提供建造和验证符合空勤人员训练要求的、足够逼真的飞行模拟器所必须的数据范围和内容。　　本标准不是确定飞行模拟器数据要求的唯一方法。

Data Requirements for Flight Simulator Design and Performance Powerplant Systems

ICS
CCS: V72
发布: 1996-09-13
实施: 1997-10-01

SAE AIR5006/2-1996 固体火箭助推器可靠性指南.第二卷的固体火箭助推器的概率设计和分析方法

The authors of this guidebook and the solid propulsion industry at large have long been troubled by an inability to absolute demonstrate SRB reliability because, under classic reliability theory, large numbers of tests are required to establish statistically significant reliability values. 240 tests with no failures, for instance, are required to demonstrate 0.99 reliability to a 90% confidence level if a binomial model is used. Since the testing cost for hundreds of large motors like space shuttle SRBs would be prohibitive, the solids industry has always been confronted with a vexing dilemma: (1) what is the fewest number of SRBs that can be tested to establish reliability with high confidence level for commitment to flight and (2) what should the reliability that was established with fewer-than- classical numbers of tests be called (it obviously is not demonstrated reliability in the strictest sense of the definition)?

Solid Rocket Booster Reliability Guidebook - Volume II Probabilistic Design and Analysis Methods for Solid Rocket Boosters

ICS: 49.050
CCS: V72
发布: 1996-06-01
实施

SAE ARP4900-1996 用液体燃料推进的火箭发动机可靠性认证

Current design and development practices leading to formal liquid rocket engine qualification (USAF) or certification (NASA) will not achieve the specific reliability objectives of future programs. New rocket engine programs are dictating quantified requirements for high reliability in parallel with a cost-constrained procurement environment. These specified reliability levels cannot be validated with the necessary confidence in a timely or cost-effective manner by present methods. Therefore, a new improved process is needed and has been developed. This new reliability certification method will be discussed in detail in the five sections that comprise this document. Primary purposes of this report are to: a. define and illustrate this process; b. point out its strengths and weaknesses; and c. provide guidelines for its application on programs which have specified reliability requirements.

Liquid Rocket Engine Reliability Certification [Superseded: SAE ARD 50009]