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Results of an On-Going Long Duration Ground Test of the DS1 Flight Spare EngineGround testing of the DS1 night spare thruster (FT2) is presently being conducted. To date, the thruster has accumulated over 4500 hours of operation. Comparison of FT2 with the performance of the engineering model thruster 2 (EMT2) during the 8.2 khr test shows a transient, lasting for about 3000 hours, during which the discharge chamber efficiency decreases for both thrusters. The flow rates are 2% lower for FT2 than for EMT2 and the discharge chamber performance is 4.5% lower for FT2 during the transient. Sensitivity data obtained during the test show that the lower flow rate accounts for about half of the observed difference. After the initial transients decay, the performance of both thrusters is comparable with the exception of the electron backstreaming margin--which is 6 V lower for FT2.
Document ID
20000058163
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
Authors
Anderson, John R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Goodfellow, Keith D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Polk, James E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Shotwell, Robert F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Rawlin, Vincent K.
(NASA Glenn Research Center Cleveland, OH United States)
Sovey, James S.
(NASA Glenn Research Center Cleveland, OH United States)
Patterson, Michael J.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
JPC-99-2857
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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