NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Development of a liquid-fed water resistojetA concept for a forced-flow once-through water vaporizer for application to resistojet thrusters was evaluated as an element of a laboratory model thruster and tested to investigate its operating characteristics. The vaporizer design concept employs flow swirling to attach the liquid flow to the boiler chamber wall, providing for separation of the two liquid phases. This vaporizer was modified with a nozzle and a centrally-located heater to facilitate vaporization, superheating, and expansion of the propellant, allowing it to function as a resistojet. Performance was measured at thrust levels ranging from 170 to 360 mN and at power levels ranging from 443 to 192 W. Maximum measured specific impulse was 192 sec.
Document ID
19880015584
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morren, W. Earl
(NASA Lewis Research Center Cleveland, OH, United States)
Stone, James R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA PAPER 88-3288
NAS 1.15:100927
E-4192
NASA-TM-100927
Report Number: AIAA PAPER 88-3288
Report Number: NAS 1.15:100927
Report Number: E-4192
Report Number: NASA-TM-100927
Accession Number
88N24968
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available