DocumentCode :
2061742
Title :
Mars sample return Orbiter/Earth Return Vehicle technology needs and mission risk assessment
Author :
Dankanich, John W. ; Burke, Laura M. ; Hemminger, Joseph A.
Author_Institution :
Gray Res., Inc., Cleveland, OH, USA
fYear :
2010
fDate :
6-13 March 2010
Firstpage :
1
Lastpage :
11
Abstract :
For many years, NASA and the science community have been asking for a Mars Sample Return (MSR) mission. There have been numerous studies to evaluate MSR mission architectures, technology needs and development plans, and top-level requirements. Because of the challenges, technologically and financially, of the MSR mission, NASA initiated a study top-level look at MSR propulsion technologies through the In-Space Propulsion Technology (ISPT) project office. The impact of propulsion technologies of the MSR Orbiter/Earth Return Vehicle (ERV) are evaluated for performance and overall mission risk. Technology trades included advanced bi-propellant engines, electric propulsion, and aerobraking. Results are presented herein.
Keywords :
aerospace engines; aerospace propulsion; planetary rovers; propellants; space research; space vehicles; ISPT project; MSR Orbiter/Earth Return Vehicle technology; MSR mission architecture; MSR propulsion technology; Mars Sample Return Orbiter; aerobraking; bipropellant engines; development plans; electric propulsion; in-space propulsion technology; mission risk assessment; technology needs; top-level requirements; Chemical technology; Costs; Earth; Mars; NASA; Propulsion; Risk management; Service oriented architecture; Space technology; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2010 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-3887-7
Electronic_ISBN :
1095-323X
Type :
conf
DOI :
10.1109/AERO.2010.5446767
Filename :
5446767
Link To Document :
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