DocumentCode :
2792114
Title :
SHERPA: A Flexible & Responsive Small Satellite Transport Vehicle
Author :
Fram, Lt Bryan ; Sauter, Lt Luke ; Buckley, Steven ; Summers, Bob ; Rogers, Aaron
Author_Institution :
Kirtland Air Force Base, Albuquerque, NM
fYear :
2005
fDate :
5-12 March 2005
Firstpage :
1
Lastpage :
8
Abstract :
SHERPA1,2, the Shuttle Expendable Rocket for Payload Augmentation, is a highly capable propulsive satellite. The SHERPA is currently approaching a PDR level design. The SHERPA can perform a wide range of missions including orbit transfers, small satellite maneuvers, space situational awareness missions, and serve as a platform for experiments. The SHERPA has three versions: The Mark I, is a propulsion unit, the Mark II is a standalone propulsive satellite, and the Mark III, a self contained long-duration propulsive satellite. Each version can support either an electric or chemical propulsion module. The SHERPA integrates several Air Force Research Laboratory developed technologies into one unique package. The SHERPA can also fulfil a number of other mission needs as a low cost satellite bus for the DoD Space Test Program
Keywords :
aerospace propulsion; artificial satellites; space research; Mark I propulsion unit; Mark II standalone propulsive satellite; Mark III self contained long-duration propulsive satellite; SHERPA; orbit transfers; payload augmentation; satellite maneuvers; shuttle expendable rocket; small satellite transport vehicle; space situational awareness missions; Chemicals; Laboratories; Payloads; Propulsion; Rockets; Satellites; Space missions; Space shuttles; Space technology; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2005 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
0-7803-8870-4
Type :
conf
DOI :
10.1109/AERO.2005.1559583
Filename :
1559583
Link To Document :
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