Abstract: This standard establishes requirements for the design and test of all pressurized systems for missiles, space vehicles and ground support equipment. These requirements, when implemented on a particular pressurized system, ...

Abstract: According to the U.S. Government Orbital Debris Standard Practices, a spacecraft or upper stage with perigee altitude below 2000 km in its final mission orbit may be disposed of by using an atmospheric reentry option. The guideline for atmospheric reentry is stated as follows:
"Leave the structure in an orbit in which, using conservative projec...

Abstract: This standard establishes procedures under which the contractor will provide spare parts, inventory and maintenance services for space and missile systems.

Abstract: Purpose
This TOR establishes requirements and guidelines for the development, testing, storage, handling, and usage of lithium-ion cells and batteries for launch vehicle applications, including booster ...

Abstract: This standard establishes requirements for the storage, handling, and usage of nickel-cadmium batteries for space vehicle applications. Compliance with this standard is intended to assure proper performance of nickel-cadmium ...

Abstract: Purpose
The purpose of this standard is to establish uniform requirements for software development activities.
Application²
This standard applies to the development ...

Abstract: Purpose
This document shall be used for tailoring the AIAA Standard, S-120-2006 dated 1 December 2006, to provide effective program execution and mission success.
Application ...

Abstract: PURPOSE
This standard establishes the electromagnetic compatibility requirements for space systems, including frequency management, and the related requirements for the electrical and electronic ...

Abstract: This handbook provides guidance for establishing uniform procedures for the control, determination, and documentation of product verification test requirements for launch, upper-stage, and space vehicles.