NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Ames Hybrid Combustion FacilityThe report summarizes the design, fabrication, safety features, environmental impact, and operation of the Ames Hybrid-Fuel Combustion Facility (HCF). The facility is used in conducting research into the scalability and combustion processes of advanced paraffin-based hybrid fuels for the purpose of assessing their applicability to practical rocket systems. The facility was designed to deliver gaseous oxygen at rates between 0.5 and 16.0 kg/sec to a combustion chamber operating at pressures ranging from 300 to 900. The required run times were of the order of 10 to 20 sec. The facility proved to be robust and reliable and has been used to generate a database of regression-rate measurements of paraffin at oxygen mass flux levels comparable to those of moderate-sized hybrid rocket motors.
Document ID
20030054522
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Zilliac, Greg
(NASA Ames Research Center Moffett Field, CA, United States)
Karabeyoglu, Mustafa A.
(Stanford Univ. Stanford, CA, United States)
Cantwell, Brian
(Stanford Univ. Stanford, CA, United States)
Hunt, Rusty
(NASA Ames Research Center Moffett Field, CA, United States)
DeZilwa, Shane
(NASA Ames Research Center Moffett Field, CA, United States)
Shoffstall, Mike
(White Sands Test Facility Las Cruces, NM, United States)
Soderman, Paul T.
(NASA Ames Research Center Moffett Field, CA, United States)
Bencze, Daniel P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2003
Subject Category
Propellants And Fuels
Report/Patent Number
A-0309067
NAS 1.15:211864
NASA/TM-2003-211864
Report Number: A-0309067
Report Number: NAS 1.15:211864
Report Number: NASA/TM-2003-211864
Funding Number(s)
CONTRACT_GRANT: NCC2-1300
OTHER: 714-04-00
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available