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Qualification evaluation of the tower jettison motor for the Apollo spacecraft program launch escape system
NTRS Full-Text: Click to View  [PDF Size: 5.2 MB]
Author and Affiliation:
Lee, B. J.(NASA Lyndon B. Johnson Space Center, Houston, TX, United States)
Abstract: Qualification tests of tower jettison motors for Apollo spacecraft program launch escape systems
Publication Date: Mar 01, 1971
Document ID:
19710015557
(Acquired Nov 22, 1995)
Accession Number: 71N25033
Subject Category: PROPULSION SYSTEMS
Report/Patent Number: NASA-TN-D-6295, MSC-S-216
Document Type: Technical Report
Publisher Information: WASHINGTON, United States
Contract/Grant/Task Num: 914-50-60-01-72
Financial Sponsor: NASA; United States
Organization Source: NASA Johnson Space Center; Houston, TX, United States
Description: 111p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: APOLLO PROJECT; ENGINE TESTS; LAUNCH ESCAPE SYSTEMS; SOLID PROPELLANT ROCKET ENGINES; APOLLO SPACECRAFT; ENVIRONMENTAL TESTS; JETTISON SYSTEMS; POLYSULFIDES; STATIC FIRING
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