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Characterization of real gas properties for Space Shuttle main engine fuel turbine and performance c

Harloff, G. J. (Gary James), 1945-
Cleveland, Ohio : Sverdrup Technology, Inc., Lewis Research Center, [1986] 1986

Design and analysis report for the RL 10-2B breadboard low thrust engine final report

Brown, James R.
West Palm Beach, FL : United Technologies Corporation, Pratt & Whitney, Government Products Division, [1984] 1984

Hybrid propulsion technology program. final report

San Jose, CA : United Technologies Chemical Systems ; Marshall Space Flight Center, AL : George C. Marshall Space Flight Center, National Aeronautics and Space Administration, [1989] 1989

Hybrid propulsion technology program.

San Jose, CA : United Technologies Chemical Systems ; Marshall Space Flight Center, AL : George C. Marshall Space Flight Center, National Aeronautics and Space Administration, [1989] 1989

Improved two-dimensional-kinetics computer program second quarterly progress report, 1 April 1984 th

Nickerson, Gary R.
Santa Ana, Calif. : Software and Engineering Associates, Inc. ; [Washington, D.C. : National Aeronautics and Space Administration, 1984?] 1984

Metallized gelled propellants : oxygen/RP-1/aluminum rocket heat transfer and combustion measurement

Palaszewski, Bryan Alan Richard, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996. 1996-

NSTAR ion thruster and breadboard power processor functional integration test results

Hamley, John A., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996. 1996-

The problem of space travel the rocket motor

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995] 1995

QM-8 field joint protection system final report

Hale, Elgie.
Brigham City, Utah : Morton Thiokol, Inc., Space Division ; [Washington, D.C. : National Aeronautics and Space Administration, 1989- 1989

QM-8 final performance evaluation report.

Nelsen, Lowell V.
Brigham City, UT : Thiokol Corp., Space Operations ; Marshall Space Flighjt Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1989]. 1989

RL10A-3-3A rocket engine modeling project

Binder, Michael, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1997. 1997-

Rocket-based combined cycle engine technology development : inlet CFD validation and application

DeBonis, James R., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996. 1996-

Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber

Wadel, Mary F., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, June 1996. 1996-

Nanomaterials in rocket propulsion systems

Amsterdam, Netherlands : Elsevier, [2019] 2019

Risk assessment and scaling for the SLS LH2 ET

Osipov, Viatcheslav (Slava), author.
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, 2012. 2012