Assessing Cost Drivers for Mars Small Spacecraft Missions

被引:2
|
作者
Edwards, Charles D., Jr. [1 ]
Fleischer, Samuel R. [1 ]
Austin, Alex [1 ]
Barba, Nathan J. [1 ]
Bjornstad, Patrick [1 ]
Woolley, Ryan C. [1 ]
Hihn, Jairus M. [1 ]
Kolanjian, Anto [1 ]
Saing, Michael [1 ]
Lock, Robert [1 ]
机构
[1] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
来源
2022 IEEE AEROSPACE CONFERENCE (AERO) | 2022年
关键词
D O I
10.1109/AERO53065.2022.9843293
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Within the Mars science community, there is growing interest in the role that small spacecraft missions can play in increasing the breadth and frequency of Mars exploration. Fueled by significant advances in miniaturization of science instruments and avionics, innovative concepts for delivery of small spacecraft to Mars, and emerging low-cost capabilities in the fast-growing NewSpace marketplace, small spacecraft missions appear capable of achieving compelling Mars science results at unprecedentedly low mission cost, far below the current NASA Discovery Program cost cap. We report on the development of a cost model for small spacecraft Mars orbiters, providing insight into the dependence of mission cost on key mission parameters, including science payload characteristics (e.g., mass, power), mission design parameters (e.g., Delta V), and mission risk categorization. These results can help guide NASA and others in establishing budget guidelines for a new class of low-cost, small spacecraft missions.
引用
收藏
页数:12
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