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Record Details

Record 30 of 4130
Optimum design of space storable gas/liquid coaxial injectors.
Author and Affiliation:
Burick, R. J.(North American Rockwell Corp., Rocketdyne Div., Canoga Park, Calif., United States)
Abstract: Review of the results of a program of single-element, cold-flow/hot-fire experiments performed for the purpose of establishing design criteria for a high-performance gas/liquid (FLOX/CH4) coaxial injector. The approach and the techniques employed resulted in the direct design of an injector that met or exceeded the performance and chamber compatibility goals of the program without any need for the traditional 'cut-and-try' development methods.
Publication Date: Nov 01, 1972
Document ID:
19730028598
(Acquired Dec 04, 1995)
Accession Number: 73A13400
Subject Category: PROPULSION SYSTEMS
Report/Patent Number: AIAA PAPER 72-1076
Document Type: Conference Paper
Publisher Information: United States
Meeting Information: Joint Propulsion Specialist Conference; 8th; Nov. 29-Dec. 1, 1972; New Orleans, LA; US
Meeting Sponsor: American Institute of Aeronautics and Astronautics;
Society of Automotive Engineers
Contract/Grant/Task Num: NAS3-12051
Financial Sponsor: NASA; United States
Description: 12p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: Copyright
NASA Terms: COAXIAL FLOW; GAS-LIQUID INTERACTIONS; INJECTORS; ROCKET ENGINE DESIGN; SPACE STORAGE; COLD FLOW TESTS; CORE FLOW; FLOX; FUEL INJECTION; HYDROCARBON FUELS; TEST FIRING
Imprint And Other Notes: American Institute of Aeronautics and Astronautics and Society of Automotive Engineers, Joint Propulsion Specialist Conference, 8th, New Orleans, La., Nov. 29-Dec. 1, 1972, AIAA 12 p.
Availability Source: Other Sources
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