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Record Details

Record 10 of 12903
Overview of Liquid Propellant Rocket Engine Systems and the J-2X
NTRS Full-Text: Click to View  [PDF Size: 993 KB]
Author and Affiliation:
Ballard, Richard O.(NASA Marshall Space Flight Center, Huntsville, AL, United States)
Abstract: No abstract available
Publication Date: Jun 04, 2011
Document ID:
20120016652
(Acquired Dec 10, 2012)
Subject Category: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Report/Patent Number: M11-0632
Document Type: Oral/Visual Presentation
Financial Sponsor: NASA Marshall Space Flight Center; Huntsville, AL, United States
Organization Source: NASA Marshall Space Flight Center; Huntsville, AL, United States
Description: 32p; In English; Original contains black and white illustrations
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: UPPER STAGE ROCKET ENGINES; GENERAL OVERVIEWS; LIQUID PROPELLANT ROCKET ENGINES; LIQUID ROCKET PROPELLANTS; ROCKET ENGINE DESIGN; STORABLE PROPELLANTS; NOZZLE DESIGN; CRYOGENIC ROCKET PROPELLANTS; MONOPROPELLANTS
Miscellaneous Notes: Invited lecture on July 4-8, 2012 at the University of Stuttgart, Stuttgart, Germany
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