DocumentCode
2099313
Title
Continuing evolution of Mars sample return
Author
Mattingly, Richard ; Matousek, Steve ; Jordan, Frank
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
1
fYear
2004
fDate
6-13 March 2004
Abstract
In 2001, JPL commissioned four industry teams to make a fresh examination of Mars Sample Return (MSR) mission architectures. As new fiscal realities of a cost-capped Mars Exploration Program unfolded, it was evident that the converged-upon MSR concept did not fit reasonably within a balanced program. Therefore, along with a new MSR Science Steering Group, JPL asked the industry teams plus JPL\´s Team-X to explore ways to reduce the cost. A paper presented at last year\´s conference described the emergence of a new, affordable "Groundbreaking-MSR" concept (Mattingly et al., 2003). This work addresses the continued evolution of the Groundbreaking MSR concept over the last year. One of the tenets of the low-cost approach is to use substantial heritage from an earlier mission, Mars Science Laboratory (MSL). Recently, the MSL project developed and switched its baseline to a revolutionary landing approach, coined "skycrane" where the MSL, which is a rover, would be lowered gently to the Martian surface from a hovering vehicle. MSR has adopted this approach in its mission studies, again continuing to capitalize on the heritage for a significant portion of the new lander. In parallel, a MSR Technology Board was formed to reexamine MSR technology needs and participate in a continuing refinement of architectural trades. While the focused technology program continues to be definitized through the remainder of this year, the current assessment of what technology development is required, is discussed in this paper. In addition, the results of new trade studies and considerations will be discussed. Adopting these changes, the Groundbreaking MSR concept has shifted to that presented in this paper. It remains a project that is affordable and meets the basic science needs defined by the MSR Science Steering Group in 2002.
Keywords
Mars; planetary rovers; planetary surfaces; space vehicles; Groundbreaking MSR concept; MSR Science Steering Group; MSR Technology Board; Mars Exploration Program; Mars Science Laboratory; Mars sample return mission architecture; Martian surface; planetary rover; revolutionary landing; skycrane; Costs; Laboratories; Mars; NASA; Postal services; Propulsion; Solar system; Space missions; Space technology; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1367630
Filename
1367630
Link To Document