DocumentCode :
2910214
Title :
Simple, robust cryogenic propellant depot for near term applications
Author :
McLean, Christopher ; Pitchford, Brian ; Mustafi, Shuvo ; Wollen, Mark ; Walls, Laurie ; Schmidt, Jeff
Author_Institution :
Ball Aerosp. & Technol. Corp., Boulder, CO, USA
fYear :
2011
fDate :
5-12 March 2011
Firstpage :
1
Lastpage :
24
Abstract :
The ability to refuel cryogenic propulsion stages on-orbit provides an innovative paradigm shift for space transportation supporting National Aeronautics and Space Administration´s (NASA) Exploration program as well as deep space robotic, national security and commercial missions. Refueling enables large beyond low Earth orbit (LEO) missions without requiring super heavy lift vehicles that must continuously grow to support increasing mission demands as America´s exploration transitions from early Lagrange point missions to near Earth objects (NEO), the lunar surface and eventually Mars. Earth-to-orbit launch can be optimized to provide competitive, cost-effective solutions that allow sustained exploration.
Keywords :
aerospace instrumentation; cryogenics; propellants; NASA Exploration program; cryogenic propulsion; low Earth orbit missions; robust cryogenic propellant depot; space transportation; Cryogenics; Earth; Low earth orbit satellites; NASA; Propulsion; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-7350-2
Type :
conf
DOI :
10.1109/AERO.2011.5747488
Filename :
5747488
Link To Document :
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