DocumentCode :
1886081
Title :
Systems engineering and support systems technology considerations of a Mars Ascent Vehicle
Author :
Sengupta, Anita ; Pauken, Michael ; Kennett, Andrew ; Trinidad, Mark ; Zabrensky, Ed
Author_Institution :
Jet Propulsion Lab., Pasadena, CA, USA
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
11
Abstract :
A Mars Ascent Vehicle (MAV) systems engineering study is underway to define the driving requirements, concept of operations, system engineering challenges, and surface support systems to enable the launch of a rock core sample to a specified delivery orbit for later retrieval and return to Earth. The proposed MAV would essentially be a small-scale launch vehicle, the first of its kind to be launched autonomously from another planet. The MAV would be a flight element of the proposed Mars Sample Return (MSR) campaign architecture, which currently assumes a 2018 launch of the sample caching mission and a 2024 (Earth) launch date of the MAV and lander, with arrival on Mars in 2025. After 9 months on the surface the MAV would be erected and launched to a specified delivery orbit. In the delivery orbit it would release its payload, a 5 kg sphere containing the rock core sample. An orbiter would rendezvous and capture the payload, returning it to Earth a year later.
Keywords :
Earth orbit; Mars; aerospace materials; aerospace simulation; rocks; space vehicles; Earth; Mars ascent vehicle; Mars sample return; caching mission; flight element; rock core sample; small-scale launch vehicle; specified delivery orbit; support systems technology; surface support systems; systems engineering; Construction; Electron tubes; Engines; Mars; Orbits; Propulsion; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187298
Filename :
6187298
Link To Document :
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