DocumentCode
1878038
Title
Entry, Descent, and Landing performance trades to increase landed mass for the Mars 2018 mission
Author
Winski, Richard ; García-Llama, Eduardo ; Prakash, Ravi ; Shidner, Jeremy ; Grover, Myron R. ; Ivanov, Mark
Author_Institution
Binera, Inc., Yorktown, VA, USA
fYear
2012
fDate
3-10 March 2012
Firstpage
1
Lastpage
13
Abstract
The proposed Mars 2018 mission is a joint mission with the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA) that is currently in the early study phase. The objective would be to land a rover which caches a sample of Martian soil for retrieval and potential return to Earth on a subsequent mission. The Mars 2018 Entry, Descent, and Landing (EDL) system would largely leverage off of heritage from the Mars Science Laboratory (MSL) EDL system in an effort to minimize cost and schedule risk. Despite the desire to have high MSL heritage, a series of trade studies were performed to quantify the impact that incorporating EDL technologies would have on the landed mass. These new technologies include a trim tab, an increased diameter disk-gap-band (DGB) parachute over MSL, a large ringsail parachute, and a supersonic inflatable aerodynamic decelerator (SIAD).
Keywords
Mars; aerodynamics; aerospace instrumentation; parachutes; planetary rovers; DGB parachute; EDL system; ESA; Earth; European Space Agency; Mars 2018 mission; Mars Science Laboratory; Martian soil; NASA; National Aeronautics and Space Administration; descent performance; disk-gap-band parachute; entry performance; landed mass; landing performance; ringsail parachute; rover landing; supersonic inflatable aerodynamic decelerator; Aerodynamics; Analytical models; Atmospheric modeling; Mars; Mathematical model; NASA; 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.2012.6186998
Filename
6186998
Link To Document