Sample Return Container Opening Process Concept for Potential Mars Sample Return

被引:1
|
作者
Strahle, Jackson W. [1 ]
Mock, Stephen [1 ]
Mattingly, Richard [1 ]
Younse, Paulo [1 ]
Chesin, Jake [1 ]
Kim, Tae [1 ]
Mayo, John [1 ]
Lengtat, Clifford [1 ]
Liu, Yang [1 ]
机构
[1] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
关键词
D O I
10.1109/AERO50100.2021.9438243
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Proposed Mars Sample Return (MSR) missions would require a pristine and secure opening method to ensure sample Contamination Control and backward Planetary . Protection. In order to reach the samples, a series of five containers would need to be opened inside of a Mars Returned Sample Handling (MRSH) facility. The process would include opening the Containment Assurance Module (CAM) aboard the Earth Entry Vehicle (EEV), the Secondary Containment Vessel (SCV), Primary Containment Vessel (PCV), and the Orbiting Sample (OS) container, and finally removing and opening the Returned Sample Tube Assemblies (RSTA). Some of these containers can be opened by reversing the mechanical assembly process Is hile, others would require destructive means. Several containers are still in a conceptual design phase, while others are en route to Mars aboard the M2020 rover. In order to inform the design of the containers that are still in the conceptual stages, a study was performed at each level of the containment assembly. The studies were used to determine the least destructive and most robust methods to disassemble and open the containers while minimizing risk to the samples or the personnel. In addition to the envisioned disassembly and breaching method, contingency plans were made for completing the disassembly if damage to the vehicle and containment system occurred.
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页数:19
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