Name: NASA STD 7003 : 2011
Brand: NASA

PYROSHOCK TEST CRITERIA

Published date

01-01-2011

Publisher

National Aeronautics and Space Administration

DOCUMENT HISTORY LOG
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. ACRONYMS, SYMBOLS AND DEFINITIONS
4. REQUIREMENTS
APPENDICES
A - Prediction of Pyroshock Environments
B - Determination of Maximum Expected Flight Environment
C - Guidance

Specifies a consistent methodology for developing pyroshock test criteria for NASA spacecraft, payload, and launch vehicle hardware during the development, qualification (Qual), flight acceptance (FA), and/or protoflight (PF) test phases of the verification process.

DocumentType	Standard
PublisherName	National Aeronautics and Space Administration
Status	Current

BS ISO 19683:2017	Space systems. Design qualification and acceptance tests of small spacecraft and units
ISO 19683:2017	Space systems — Design qualification and acceptance tests of small spacecraft and units
NASA HDBK 7008 : 2014	SPACECRAFT DYNAMIC ENVIRONMENTS TESTING
AECTP-400 : 2006	MECHANICAL ENVIRONMENTAL TESTS
NASA GSFC STD 7000 : 2013	GENERAL ENVIRONMENTAL VERIFICATION STANDARD (GEVS) FOR GSFC FLIGHT PROGRAMS AND PROJECTS
16/30302535 DC : 0	BS ISO 19683 - SPACE SYSTEMS - DESIGN QUALIFICATION AND ACCEPTANCE TESTS OF SMALL SPACECRAFT AND UNITS
NASA MSFC STD 3676 : 2013	DEVELOPMENT OF VIBROACOUSTIC AND SHOCK DESIGN AND TEST CRITERIA

IEST RP DTE032.2 : 2009	PYROSHOCK TESTING TECHNIQUES
NASA HDBK 7005 : 2001	DYNAMIC ENVIRONMENTAL CRITERIA
NASA STD 7002 : 0	PAYLOAD TEST REQUIREMENTS
ISO 18431-4:2007	Mechanical vibration and shock Signal processing Part 4: Shock-response spectrum analysis
NASA STD 8719.12 : 2010	SAFETY STANDARD FOR EXPLOSIVES, PROPELLANTS, AND PYROTECHNICS