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Performance of a 10 mlb biowaste resistojet.Description of the thrusting performance of a 10-mlb thrust, concentric-tubes biowaste resistojet, which was life tested on hydrogen and ammonia propellants for 8000 hours. Thrusting performance is presented for H2, H2O, CH4, and CO2 as well as typical biopropellant mixtures CO2-CH4, H2O-CH4 and CO2-H2O. Using Pt-Ir alloy heater tubes, 235 and 575 seconds were obtained for water and hydrogen propellants. Overall total power efficiencies were 66%, which includes losses for a preevaporator close-coupled for the water tests. Vibration to 1.0 sq q/Hz with an overall G rms of 36, shock at 30 g's and acceleration to 8 g's simulating a launch were passed by the thrustor.
Document ID
19720026597
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Phillips, D. G.
(Marquardt Co. Van Nuys, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
SAE PAPER 710769
Accession Number
72A10263
Funding Number(s)
CONTRACT_GRANT: NAS1-9474
Distribution Limits
Public
Copyright
Other

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