ASTM E1997-99 - 10.1.1999
 
1. Scope

1.1 The purpose of this practice is to aid engineers, designers, quality and reliability control engineers, materials specialists, and systems designers in the selection and control of materials and processes for spacecraft, external portion of manned systems, or man-tended systems. Spacecraft systems are very different from most other applications. Space environments are very different from terrestrial environments and can dramatically alter the performance and survivability of many materials. Reliability, long life, and inability to repair defective systems (or high cost and difficulty of repairs for manned applications) are characteristic of space applications. This practice also is intended to identify materials processes or applications that may result in degraded or unsatisfactory performance of systems, subsystems, or components. Examples of successful and unsuccessful materials selections and uses are given in the appendices.

 
2. Referenced Documents

G64-99(2021)

Standard Classification of Resistance to Stress-Corrosion Cracking of Heat-Treatable Aluminum Alloys

PSS-07/QRM-0

Guidelines for Space Materials Selection European Space Agency, 810, Rue Mario-Nikis, 75738 Paris Cedex, France.

E595-15(2021)

Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment

MIL-HDBK-17

Properties of Composite Materials

MIL-HDBK-5

MIL-STD-889

MSFC-STD-3029

Guidelines to the Selection of Metallic Materials for Stress Corrosion Cracking Resistance in Sodium Chloride Environments Marshall Space Flight Center, AL 35812, or everyspec.com.