Hypervelocity impact testing of the pressurized mating adapters for the International Space Station-Reference-Cited by-同舟云学术

Hypervelocity impact testing of the pressurized mating adapters for the International Space Station

Published:1999-12 Issue:1 Volume:23 Page:215-224
ISSN:0734-743X
Container-title:International Journal of Impact Engineering
language:en
Short-container-title:International Journal of Impact Engineering

Author:

Dvorak Bruce D.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference14 articles.

1. Boeing Space Station Division, Pressurized Mating Adapter Prime Item Development Specifications (PIDS) S684-10115E (06 Oct 1997) and SP-M-301H (06 Oct 1997), Section 3.3.12.1.16.1.

2. Boeing Space Station Division, Pressurized Mating Adapters Structural Integrity Report (FCA/PCA Submittal);Report No. MDC 95H0336,1997

3. Boeing Space Station Division, Pressurized Mating Adapter Prime Item Development Specifications (PIDS) S684-10115E (06 Oct 1997) and SP-M-301H (06 Oct 1997), Section 3.3.12.1.3.1.

4. NASA-Johnson Space Center Hypervelocity Impact Test Facility, Phase-I Pressurized Mating Adapter Hypervelocity Impact Pre-Declared Development;Report No. JSC 27131,1995

5. NASA-Johnson Space Center Hypervelocity Impact Test Facility, Phase-II Hypervelocity Impact Pre-Declared Development Testing of Pressurized Mating Adapter Meteoroid/Orbital Debris Shield;Report No. JSC 26967,1996

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