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Engineering the Future of Full-Scale Propulsion TestingYear 2000 has been an active one for rocket propulsion testing at the NASA John C. Stennis Space Center. This paper highlights several major test facilites for large-scale propulsion devices, and summarizes the varied nature of the recent test projects conducted at the Stennis Space Center (SSC) such as the X-33 Aerospike Engine, Ultra Low Cost Engine (ULCE) thrust chamber program, and the Hybrid Sounding Rocket (HYSR) program. Further, an overview of relevant engineering capabilities and technology challenges in conducting full-scale propulsion testing are outlined.
Document ID
20030107869
Acquisition Source
Stennis Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ryan, H. M.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Solano, W.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Holland, R.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Saint Cyr, W.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Rahman, S.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Date Acquired
September 7, 2013
Publication Date
January 2, 2001
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
SE-2001-01-00001-SSC
AIAA Paper 2001-0746
Report Number: SE-2001-01-00001-SSC
Report Number: AIAA Paper 2001-0746
Meeting Information
Meeting: 39th AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 8, 2001
End Date: January 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available