Liquid Propulsion Systems - Evolution and Advancements

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Liquid Propulsion Systems - Evolution and Advancements
NTRS Full-Text: Click to View [PDF Size: 7.1 MB]
Author and Affiliation:
Ballard, Richard O.
(NASA Marshall Space Flight Center, Huntsville, AL, United States)[/t][/t]

Abstract: No abstract available
Publication Date: Jul 15, 2013
Document ID: 20140002716 (Acquired Apr 09, 2014)
Subject Category:[/t]
PROPELLANTS AND FUELS; SPACECRAFT PROPULSION AND POWER; LAUNCH VEHICLES AND LAUNCH OPERATIONS
Report/Patent Number: M13-2799
Document Type: Oral/Visual Presentation
Meeting Information: AIAA/ASME/SAE/ASEE Joint Propulsion Conference; 49th; 15-18 Jul. 2013; San Jose, CA; United States
Meeting Sponsor: American Inst. of Aeronautics and Astronautics; Liquid Propulsion Technical Committee; Los Angeles, CA, United States
Financial Sponsor: NASA Marshall Space Flight Center; Huntsville, AL, United States
Description: 112p; In English; Original contains color and black and white illustrations
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: PROPULSION SYSTEM CONFIGURATIONS; PROPULSION SYSTEM PERFORMANCE; LIQUID PROPELLANT ROCKET ENGINES; LIQUID ROCKET PROPELLANTS; ROCKET THRUST; SPECIFIC IMPULSE; PROPELLANT MASS RATIO; RADIANT FLUX DENSITY; X-15 AIRCRAFT
Miscellaneous Notes: AIAA Professional Development Short Course
 
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