Colloid Thruster for Attitude Control Systems (ACS) and Tip-off Control Applications

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,981.00
Award Year:
2009
Program:
SBIR
Phase:
Phase II
Contract:
NNX09CA81C
Award Id:
88154
Agency Tracking Number:
075294
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
11 Tech Circle, Natick, MA, 01760
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
185739591
Principal Investigator:
NathanielDemmons
Principal Investigator
(508) 655-5565
nate@busek.com
Business Contact:
JudyBudny
Business Official
(508) 655-5565
judy@busek.com
Research Institute:
n/a
Abstract
Busek proposes to develop and deliver a complete engineering model colloid thruster system, capable of thrust levels and lifetimes required for spacecraft operational tasks such as tip-off de-tumbling and attitude control. The self contained thruster system shall be capable of delivering ~75ýýN with sufficient total impulse to de-tumble spacecraft such as LISA. The proposed Phase 2 work builds upon a highly successful Phase 1 effort where the key principals of the innovation, a propellant isolation membrane and a passive capillary feed system, were unequivocally demonstrated. The proposed system is completely passive with no moving parts and requires no valves to ensure its high reliability. In order to inhibit propellant contamination prior to operation in space, a unique isolation membrane will separate propellant from the emitter. Upon heating the isolation membrane dissolves, allowing propellant from a collocated reservoir to flow forward to the electrospray thruster without contamination. The thruster consists of an array of self adjusting emission sites that are activated by application of an electric field that initiates emission. The delivered thrust is modulated by varying the applied electric field. The significant innovations of the proposed colloid thruster include: a compact, low power, modular thruster system containing no moving parts, which is capable of delivering sufficient thrust for spacecraft tip-off control and ACS applications.

* information listed above is at the time of submission.

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