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High power arcjetIn this period a new mass flow controller was brought into the gas supply system, so that the upper limit for the mass flow rate could be increased up to 500 mg/s with hydrogen. A maximum specific impulse of 1500 s could be achieved with the high powered arcjet (HIPARC) at an efficiency of slightly better than 20 percent. Different nozzle throat diameters had been tested. The 100 kilo-watt input power limit was reached with the 4 mm nozzle throat diameter at a mass flow rate of 400 mg/s. Tests were carried out with different cathode gaps and with three different cathodes. In addition measurements of pressure and gas temperature were taken in the feed line in order to determine the pressure drop in the propellant injectors.
Document ID
19920013850
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goelz, T. M.
(Stuttgart Univ.)
Auweter-Kurtz, M.
(Stuttgart Univ.)
Kurtz, H. L.
(Stuttgart Univ.)
Schrade, H. O.
(Stuttgart Univ.)
Date Acquired
September 6, 2013
Publication Date
March 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-190238
NAS 1.26:190238
IRS-92-P4
Report Number: NASA-CR-190238
Report Number: NAS 1.26:190238
Report Number: IRS-92-P4
Accession Number
92N23093
Funding Number(s)
CONTRACT_GRANT: NAGW-1736
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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