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Autonomous Utility Connector for Lunar Surface Systems, Phase I

Completed

Description

Lunar dust has been identified as a significant and present challenge in future exploration missions. The interlocking, angular nature of Lunar dust and its broad grain size distribution make it particularly detrimental to mechanisms with which it may come into contact. Honeybee Robotics Spacecraft Mechanisms Corporation (HRSMC) seeks to develop a dust-tolerant, autonomous connector to transmit data and power on Lunar surface systems. HRSMC has extensive heritage in developing mechanisms for extreme and dusty environments, including the development of a dust-tolerant electrical connector prototype and a dust-tolerant mechanical connector concept. There are many near-term applications of such a connector including: the utility and electrical connections that will be used on the next-generation Lunar EVA suit, cryogenic utility connections that will be used to pass liquid hydrogen and liquid oxygen during in-situ¬ resource utilization (ISRU) activities, and high-power electrical connectors capable of thousands of cycles for Lunar Surface Mobility Unit (LSMU) battery recharge and data transfer. As noted in current Lunar architectural options, human EVA's, long range Lunar rovers, and ISRU activities are on the mission horizon and are paramount to the establishment of a permanent human base on the Moon. In Phase I, HRSMC will baseline prior dust-tolerant connector work to develop a conceptual design for an autonomous, dust-tolerant, re-usable connector to enable electrical transfer between a LSMU and a central resource outpost or a deployed solar power unit. This connector would be easily adaptable to the needs of other Lunar surface system utility connectors required for EVA suits or other systems such as ISRU utility connections. This development path will result in an autonomous Lunar dust-tolerant electrical connector with a TRL level of 3-4 at the end of Phase 1 with a goal of at least TRL 6 at the end of Phase II.

Details

Technology areaThermal Management Systems > Cryogenic Systems > Launch Vehicle Propellant
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationJohnson Space Center, Houston, TX
Start date2009-01-22
End date2009-07-22

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