Space Shuttle Main Engine program statusPerformance, weight, and reusability of the Space Shuttle Main Engine, the next generation rocket engine, are important factors in achieving the Space Shuttle mission. The design features of the engine contributing to the achievement of these engine demands are discussed. Many new fabrication methods, material applications, and innovations incorporated into the engine are presented. The engine program is now in the second year of the 47 months development period. The current status of activities in engineering, manufacturing, and test are reviewed. The Design Verification Specification approach to engine development is compared to the development programs for Saturn/Apollo engines.
Document ID
19740030169
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kirby, F. M. (Rockwell International Corp. Rocketdyne Div., Canoga Park, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 73-1177Report Number: AIAA PAPER 73-1177
Meeting Information
Meeting: Propulsion Conference
Location: Las Vegas, NV
Country: US
Start Date: November 5, 1973
End Date: November 7, 1973
Sponsors: Society of Automotive Engineers, American Institute of Aeronautics and Astronautics