SBIR/STTR Research Award

Microsatellite Direct Drive SEP Module for Interplanetary Exploration via Rideshare

Award identifier 7c54eb8d38af24a7e37b103c8b89e3ca1fac034dda3731e7e9183d7a5f5d1fa3Awarding agency National Aeronautics and Space Administration

Award amount

$124,894

Program and phase

SBIR · Phase I

Award year

2013

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ExoTerra Resource, LLC
Proposal award date
2013-05-23
Contract end date
2013-11-23
UEI
KG3LJWXMHJ25
Solicitation number
Not reported
Topic code
S3.03

Research abstract

Solar Electric Propulsion drives down the cost of space missions by using its high propulsion efficiency to step down from one launch class to another. As launch costs can be up to a third of total mission costs, stepping down to a smaller rocket can be a mission enabling technology in today's budget constrained environment.While missions such as Dawn have used this to visit multiple asteroids after launch from a small launch vehicle, ExoTerra's SolRider Direct Drive (DD) SEP module allows interplanetary missions to take the next step down in launch cost to package within standard rideshare envelope and mass contraints. Our module integrates multiple technologies to provide up to 8.6 km/s within an Atlas Aft Bulkhead Carrier rideshare or 14.6 km/s of delta-V within a standard ESPA. This can enable launch costs below $5M.Our integrated DD SEP module uses a combination of SEP technologies to create a highly efficient system to package within the rideshare envelope. We use a 175 W/kg and 60kW/m3 rolled composite tube solar array deployment system to package within the tight volume. This provides 300 V power to the thruster through a direct drive system, eliminating the cost, mass and electrical losses of the traditional power processing unit. A Hall Thruster uses the high voltage power to efficiently propel the craft with over 1600 s of Isp. The thruster receives the propellant from a cryogenic Xenon feed system, allowing an order of magnitude drop in tank mass. When coupled to Microsatellite electronics, the system can deliver up to 5.5 kg of payload instruments to Mars orbit.

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

12 SBIR/STTR records share this UEI (2013–2021). Reported award amounts total $3,311,496. 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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