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Main Engine Prototype Development for 2nd Generation RLV RS-83This presentation reports on the NASA project to develop a prototype for RS-83 engine designed for use on reusable launch vehicles (RLV). Topics covered include: program objectives, overview schedule, organizational chart, integrated systems engineering processes, requirement analysis, catastrophic engine loss, maintainability analysis tools, and prototype design analysis.
Document ID
20020085363
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
John Vilja
(Boeing (United States) Chicago, Illinois, United States)
Mark Fisher
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
September 7, 2013
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
02RS83-006
Meeting Information
Meeting: 1st AIAA/IAF Symposium on Future Reusable Launch Vehicles
Location: Huntsville, AL
Country: US
Start Date: April 12, 2002
Sponsors: American Institute of Aeronautics and Astronautics, International Astronautical Federation
Distribution Limits
Public
Copyright
Public Use Permitted.
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