This document references:
NASA-STD-5002 - LOAD ANALYSES OF SPACECRAFT AND PAYLOADS
Published by NASA
on
September 25, 2019
Purpose This NASA Technical Standard defines the methodologies, practices, and requirements for the conduct of load analyses for payloads and spacecraft and describes accepted engineering practices...
This document references:
NASA-STD-7001 - PAYLOAD VIBROACOUSTIC TEST CRITERIA
Published by NASA
on
November 7, 2017
The term “vibroacoustics” is defined as an environment induced by high-intensity acoustic noise associated with various segments of the flight profile. Vibroacoustics manifests itself throughout the...
This document references:
NASA-STD-7003 REV A - PYROSHOCK TEST CRITERIA
Published by NASA
on
December 20, 2011
Purpose The purpose of this Standard is to provide a consistent methodology for developing pyroshock test criteria for NASA spacecraft, payload, and launch vehicle hardware during the development,...
This document references:
NASA-STD-7001 - PAYLOAD VIBROACOUSTIC TEST CRITERIA
Published by NASA
on
November 7, 2017
The term “vibroacoustics” is defined as an environment induced by high-intensity acoustic noise associated with various segments of the flight profile. Vibroacoustics manifests itself throughout the...
This document references:
NASA-STD-5002 - LOAD ANALYSES OF SPACECRAFT AND PAYLOADS
Published by NASA
on
September 25, 2019
Purpose This NASA Technical Standard defines the methodologies, practices, and requirements for the conduct of load analyses for payloads and spacecraft and describes accepted engineering practices...
This document is referenced by:
AECTP-400 - MECHANICAL ENVIRONMENTAL TESTS
Published by NATO
on
November 28, 2019
PURPOSE 1. AECTP-400 is one of five documents included in STANAG 4370. It is important to use AECTP-400 with other AECTPs (100 to 500) to apply the Environmental Project Tailoring process. This...