SBIR/STTR Research Award

Dual Axis Controller for Extreme Environments

Award identifier 940b7bd2493beb2b7aa4184e5139bf69c4142fd19daa87d648f3737ced23a30aAwarding agency National Aeronautics and Space Administration

Award amount

$749,289

Program and phase

SBIR · Phase II

Award year

2016

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
MOTIV SPACE SYSTEMS, INC.
Proposal award date
2016-04-29
Contract end date
2018-06-30
UEI
R8V2M4PWLBP1
Solicitation number
Not reported
Topic code
S4.04

Research abstract

The Dual Axis Controller for Extreme Environments (DACEE) addresses a critical need of NASA's future exploration plans to investigate extreme environments within our solar system. These destinations include asteroids, comets, Phobos and Deimos, Titan, Ganymede, Mars and the Moon. Feasibility of these proposed missions is improved if subsystems can be designed to be more robust in operations and survivability such as to reduce the burden of the overall system and preserve critical resources (i.e. power and mass). In the case of DACEE, the ability to operate a functional electro-mechanical subsystem at temperatures at or below -190C addresses one of NASA's technology hurdles. In Phase 1, a two-axis compact brushless/stepper motion control design was completed with extreme cold operations maintained as the primary design driver. Individual components of the design were evaluated for risk in achieving these goals. The highest risk components were thermally tested. The results of these tests almost completely retired the risk of one component, pending further evaluation, and identified a coherent development path to remedy power regulation needs at extreme temperatures. The objectives of Phase 2 are to deliver a prototype flight-like electromechanical instrument mechanism which includes the fully developed 100 krad tolerant DACEE. This subsystem will have been cryogenically tested and characterized. The motors, gear boxes, and actuated components will be selected by leveraging the best in family for cryogenic operations. The specification of the mechanism will pay close attention to design criteria compatible with achieving significant lifetime actuation cycles based upon appropriate material selections and lubrication approaches. The objective of the Phase 2 activity is to produce a complete instrument mechanism prototype with motion control electronics capable of surviving 100 million revs at the motor.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

22 SBIR/STTR records share this UEI (2015–2025). Reported award amounts total $16,390,247. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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