NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Hypersonic Vehicle Propulsion System Control Model Development Roadmap and ActivitiesThe NASA Fundamental Aeronautics Program Hypersonic project is directed towards fundamental research for two classes of hypersonic vehicles: highly reliable reusable launch systems (HRRLS) and high-mass Mars entry systems (HMMES). The objective of the hypersonic guidance, navigation, and control (GN&C) discipline team is to develop advanced guidance and control algorithms to enable efficient and effective operation of these challenging vehicles. The ongoing work at the NASA Glenn Research Center supports the hypersonic GN&C effort in developing tools to aid the design of advanced control algorithms that specifically address the propulsion system of the HRRLSclass vehicles. These tools are being developed in conjunction with complementary research and development activities in hypersonic propulsion at Glenn and elsewhere. This report is focused on obtaining control-relevant dynamic models of an HRRLS-type hypersonic vehicle propulsion system.
Document ID
20090010395
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Stueber, Thomas J.
(NASA Glenn Research Center Cleveland, OH, United States)
Le, Dzu K.
(NASA Glenn Research Center Cleveland, OH, United States)
Vrnak, Daniel R.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2009
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-16687
NASA/TM-2009-215483
Funding Number(s)
WBS: WBS 599489.02.07.03.05.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available