DocumentCode
2910129
Title
Heavy-lift contributions to a human mission to Mars
Author
Monk, Tim ; Holladay, Jon ; Jaap, John ; Baggett, Keithe ; Pinson, Robin ; Dux, Ian ; Hopkins, Jason ; Brown, Chad
fYear
2011
fDate
5-12 March 2011
Firstpage
1
Lastpage
21
Abstract
The reference heavy-lift launch vehicle (Ares V) for NASA´s Constellation Program served as the Point of Departure for Mars Design Reference Architecture 5.0 (DRA 5.0). The Ares V vehicle consists of two 5-segment reusable solid rocket boosters, a Core Stage with five liquid oxygen/liquid hydrogen engines, and a combination upper stage and Earth Departure Stage (EDS) powered by one liquid oxygen/liquid hydrogen engine.
Keywords
Mars; aerospace instrumentation; aerospace propulsion; rocket engines; space vehicles; Ares V vehicle; DRA 5.0; Design Reference Architecture 5.0; Earth departure stage; Mars; NASA Constellation Program; core stage; heavy-lift launch vehicle; human mission; liquid oxygen/liquid hydrogen engines; solid rocket boosters; Chemicals; Low earth orbit satellites; Mars; Orbits; Payloads; Propulsion; Vehicles; 9-launch campaign; Ares V; Chemical propulsion; DRA5.0; EDS; MTV; Mars; NTP;
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.2011.5747484
Filename
5747484
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