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Design of Liquid Propellant Rocket Engines Second Edition
Document ID: 19710019929
NTRS Full-Text: Click to View  [PDF Size: 45.6 MB]
Author: Huang, D. H.; Huzel, D. K.
Abstract: Liquid propellant rocket engine conference proceedings and parameters for design of rocket engines hide
Publication Year: 1971
Document Type: Technical Report
Report/Patent Number: NASA-SP-125
Date Acquired: Nov 22, 1995
Analytical Assessment of the Reciprocating Feed System
Document ID: 20060047647
NTRS Full-Text: Click to View  [PDF Size: 2.2 MB]
Author: Eddleman, David E.; Blackmon, James B.; Morton, Christopher D.
Abstract: A preliminary analysis tool has been created in Microsoft Excel to determine deliverable payload hide
Publication Year: 2006
Document Type: Conference Paper
Date Acquired: Oct 06, 2006
Study Task for Determining the Effects of Boost-Phase Environments on Densified Propellants Thermal Conditions for Expendable Launch Vehicles
Document ID: 20020061304
NTRS Full-Text: Click to View  [PDF Size: 1.6 MB]
Author: Haberbusch, Mark S.; Meyer, Michael L. (Technical Monitor)
Abstract: A thermodynamic study has been conducted that investigated the effects of the boost-phase hide
Publication Year: 2002
Document Type: Technical Report
Report/Patent Number: NASA/CR-2002-210808, E-12715, NAS 1.26:210808
Date Acquired: Aug 02, 2002
Test Report for NASA MSFC Support of the Linear Aerospike SR-71 Experiment (LASRE)
Document ID: 20000037777
NTRS Full-Text: Click to View  [PDF Size: 6.1 MB]
Author: Elam, S. K.
Abstract: The Linear Aerospike SR-71 Experiment (LASRE) was performed in support of the Reusable Launch hide
Publication Year: 2000
Document Type: Technical Report
Report/Patent Number: NASA/TM-2000-210076, NAS 1.15:210076, M-973
Date Acquired: May 12, 2000
Reusable Launch Vehicle Tank/Intertank Sizing Trade Study
Document ID: 20000032922
NTRS Full-Text: Click to View  [PDF Size: 1.1 MB]
Author: Dorsey, John T.; Myers, David E.; Martin, Carl J.
Abstract: A tank and intertank sizing tool that includes effects of major design drivers, and which allows hide
Publication Year: 2000
Document Type: Preprint
Report/Patent Number: AIAA Paper 2000-1043
Date Acquired: Apr 28, 2000
Performance of an Axisymmetric Rocket Based Combined Cycle Engine During Rocket Only Operation Using Linear Regression Analysis
Document ID: 19980233245
NTRS Full-Text: Click to View  [PDF Size: 1.3 MB]
Author: Smith, Timothy D.; Steffen, Christopher J., Jr.; Yungster, Shaye; Keller, Dennis J.
Abstract: The all rocket mode of operation is shown to be a critical factor in the overall performance of a hide
Publication Year: 1998
Document Type: Technical Report
Report/Patent Number: NASA/TM-1998-206632, E-11090, NAS 1.15:206632
Date Acquired: Nov 21, 1998
A Rocket Engine for Mars Sample Return Using In Situ Propellants
Document ID: 19970010252
NTRS Full-Text: Click to View  [PDF Size: 951 KB]
Author: Linne, Diane L.
Abstract: Recent studies for the planned Mars sample return mission were reviewed and modified to utilize hide
Publication Year: 1997
Document Type: Conference Paper
Report/Patent Number: NASA-TM-107396, NAS 1.15:107396, AIAA-97-0893
Date Acquired: Mar 13, 1997
Stages to Saturn
Document ID: 19970009949
NTRS Full-Text: Click to View  [PDF Size: 168.10 MB]
Author: Bilstein, Roger E.
Abstract: Part one of this report is intended to bring back into focus some of the facts, circumstances, and hide
Publication Year: 1996
Document Type: Book/Monograph
Report/Patent Number: NASA-SP-4206, NAS 1.21:4206, LC-79-607154
Date Acquired: Mar 13, 1997
NASA Propulsion Engineering Research Center, Volume 2
Document ID: 19950002741
NTRS Full-Text: Click to View  [PDF Size: 61.5 MB]
Abstract: This is the second volume in the 1994 annual report for the NASA Propulsion Engineering Research hide
Publication Year: 1994
Document Type: Conference Proceedings
Report/Patent Number: NASA-CR-196312, NAS 1.26:196312, GRC-E-DAA-TN11315
Date Acquired: Dec 28, 1995
GRYPHON: Air launched space booster
Document ID: 19940020540
NTRS Full-Text: Click to View  [PDF Size: 13.2 MB]
Abstract: The project chosen for the winter semester Aero 483 class was the design of a next generation Air hide
Publication Year: 1993
Document Type: Technical Report
Report/Patent Number: NASA-CR-195497, NAS 1.26:195497
Date Acquired: Dec 28, 1995
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