SBIR/STTR Research Award

Self-Powered Electrospray Thruster Cluster for Deorbit-Detumble Applications

Award identifier 7f5281df652b69522e7dffa4682aa6f86b94c6f8e97e1f3b005f8f0f4ec37a6fAwarding agency Department of Defense · Air Force

Award amount

$99,993

Program and phase

SBIR · Phase I

Award year

2009

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
BUSEK CO., INC.
Proposal award date
2009-02-12
Contract end date
2010-02-12
UEI
SATYSBWG3FL7
Solicitation number
2008.3
Topic code
AF083-198

Research abstract

Busek Co. Inc. proposes to develop a self-powered, self-contained propulsive de-orbit system that will (a) fit within a 12 in. x 12 in. x 1 in. volume, (b) weigh less than 5kg, (c) requires no propellant tanks or valves (or any other moving parts), (d) apply torque to the spacecraft in a detumbling operational mode (e) de-orbit a 200kg asset from 700km to 200km within a 10 year period qualified.  The propulsion system is based on long life, low power electro spray thruster  Busek is uniquely poised to deliver this technology, as it has built and delivered the first space-qualified electrospray thruster to JPL (ST7-DRS program), and is the leader in developing electrospray thrusters for specific mission profiles for both NASA and the DoD. Busek is not proposing a balloon, sail, parachute or tether because in the event that a spacecraft is tumbling out of control, each of these options is subject to twisting around the spacecraft, rendering the device useless.  A deorbiting thruster cluster that can apply torque to the spacecraft, and that can sense when to burn against the orbital path, is immune to this otherwise debilitating condition.   BENEFIT: Given the growing need to develop a reliable deorbiting technology that can respond to a variety of conditions, the proposed deorbiter/detumbler thruster is promising. Initially our efforts will be to secure Phase II funding to optimize and mature the design.  A flight program is a critical goal to validate the durability and stability of the electrospray thruster operation and responsiveness to a variety of conditions. The anticipated market for the electrospray thruster package developed by this effort is expected to extend from scientific and military missions into commercial satellites. Market forecasts by Futron Corporation predict steady growth in commercial satellites. Though colloid thrusters are in a relatively early stage of product development, the team assembled for this program is world-class and on the leading edge of this technology development which includes a number of novel design features including no moving parts and the ability to operate for years continuously, with no propellant tank other than an extension of the thruster itself. This elegant design results in a simple, durable system that could be used in a variety of mission profiles and deorbit a variety of space assets up to 700km and approximately 200kg or more. We expect further development efforts could extend the range of assets that can be deorbited by this device, and be installed on every space asset of that spacecraft class that is launched.

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

248 SBIR/STTR records share this UEI (1988–2026). Reported award amounts total $87,675,405. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation

Agency intelligence

Department of Defense

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