Reliability as an Independent Variable Applied to Liquid Rocket Engine Hot Fire Test Plans
Author:
Affiliation:
1. EADS Astrium, GmbH, 81663 Munich, Germany
2. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34279
Reference38 articles.
1. Space Transportation: A Systems Approach to Analysis and Design
2. Life cycle cost considerations for launch vehicle liquid propellant rocket engines
3. Overview of United States Rocket Propulsion Technology and Associated Space Transportation Systems
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