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There are a total of 9 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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6-ft High-Power Electric Propulsion Test Port, EPL Tank 5 Installed
Author(s): Grisnik, Stanley P.; Theman, Elmer R.; Swiatek, Michael W.; Speicer, Henry J.; Jankovsky, Robert S.
Abstract: High-power electric propulsion is a critical component of NASA s proposed missions to the outer planets. Mission studies have shown that high-power, high-specific-impulse propulsion systems can deliver 2000 kg of scientific ...
NASA Center: Glenn Research Center Publication Year: 2003
Added to NTRS: 2008-06-02
Document ID: 20050215032
Scaling of Ion Thrusters to Low Power
Author(s): Patterson, Michael J.; Grisnik, Stanley P.; Soulas, George C.
Abstract: Analyses were conducted to examine ion thruster scaling relationships in detail to determine performance limits, and lifetime expectations for thruster input power levels below 0.5 kW. This was motivated by mission analyses ...
NASA Center: Glenn Research Center Publication Year: 1998
Added to NTRS: 2005-08-25
Document ID: 19980201340; Report Number: E-11010, IEPC-97-098, NAS 1.15:206530, NASA/TM-1998-206530
Experimental study of low Reynolds number nozzles
Author(s): Grisnik, Stanley P.; Smith, Tamara A.; Saltz, Larry E.
Abstract: High-performance electrothermal thrusters operate in a low nozzle-throat Reynolds number regime. Under these conditions, the flow boundary layer occupies a large volume inside the nozzle, contributing to large viscous ...
NASA Center: Glenn Research Center Publication Year: 1987
Added to NTRS: 2005-08-25
Accession Number: 87N20383; Document ID: 19870010950; Report Number: AIAA PAPER 87-0992, E-3526, NAS 1.15:89858, NASA-TM-89858
Test facilities for high power electric propulsion
Author(s): Sovey, James S.; Vetrone, Robert H.; Grisnik, Stanley P.; Myers, Roger M.; Parkes, James E.
Abstract: Electric propulsion has applications for orbit raising, maneuvering of large space systems, and interplanetary missions. These missions involve propulsion power levels from tenths to tens of megawatts, depending upon the ...
NASA Center: Glenn Research Center Publication Year: 1991
Added to NTRS: 2005-08-25
Accession Number: 92N11136; Document ID: 19920001918; Report Number: AIAA PAPER 91-3499, E-6576, NAS 1.15:105247, NASA-TM-105247
Measurement of Xenon Viscosity as a Function of Low Temperature and Pressure
Author(s): Grisnik, Stanley P.
Abstract: The measurement of xenon gas viscosity at low temperatures (175-298 K) and low pressures (350 torr-760 torr) has been performed in support of Hall Thruster testing at NASA Lewis Research Center. The measurements were taken ...
NASA Center: Glenn Research Center Publication Year: 1998
Added to NTRS: 2005-08-25
Document ID: 19980219329; Report Number: AIAA Paper 98-3498, E-11244, NAS 1.15:208409, NASA/TM-1998-208409
A large high vacuum, high pumping speed space simulation chamber for electric propulsion
Author(s): Grisnik, Stanley P.; Parkes, James E.
Abstract: Testing high power electric propulsion devices poses unique requirements on space simulation facilities. Very high pumping speeds are required to maintain high vacuum levels while handling large volumes of exhaust products. ...
NASA Center: Glenn Research Center Publication Year: 1994
Added to NTRS: 2005-08-25
Accession Number: 94N26142; Document ID: 19940021639; Report Number: E-8080, IEPC-93-151, NAS 1.15:106453, NASA-TM-106453
The effect of eddy distribution on momentum and heat transfer near the wall in turbulent pipe flow
Author(s): Zurawski, Robert L.; Grisnik, Stanley P.; Hardy, Terry L.; Ghorashi, Bahman
Abstract: A study was conducted to determine the effect of eddy distribution on momentum and heat transfer near the wall in turbulent pipe flow. The buffer zone was of particular interest in that it is perhaps the most complicated and ...
NASA Center: Glenn Research Center Publication Year: 1987
Added to NTRS: 2005-08-25
Accession Number: 88N15984; Document ID: 19880006602; Report Number: E-3882, NAS 1.15:100257, NASA-TM-100257
Test facilities for high power electric propulsion
Author(s): Sovey, James S.; Vetrone, Robert H.; Grisnik, Stanley P.; Myers, Roger M.; Parkes, James E.
Abstract: Electric propulsion has applications for orbit raising, maneuvering of large space systems, and interplanetary missions. These missions involve propulsion power levels from tenths to tens of megawatts, depending upon the ...
NASA Center: Glenn Research Center Publication Year: 1991
Added to NTRS: 2004-11-03
Accession Number: 91A52396; Document ID: 19910067773; Report Number: AIAA PAPER 91-3499
Experimental study of low Reynolds number nozzles
Author(s): Grisnik, Stanley P.; Smith, Tamara A.; Saltz, Larry E.
Abstract: High-performance electrothermal thrusters operate in a low nozzle-throat Reynolds number regime. Under these conditions, the flow boundary layer occupies a large volume inside the nozzle, contributing to large viscous ...
NASA Center: Glenn Research Center Publication Year: 1987
Added to NTRS: 2004-11-03
Accession Number: 87A41102; Document ID: 19870053828; Report Number: AIAA PAPER 87-0992
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