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Variable Thrust/Specific Impulse Electrospray Propulsion

Award Information

Agency:
Department of Defense
Branch:
Air Force
Award ID:
Program Year/Program:
2011 / STTR
Agency Tracking Number:
F08B-T09-0141
Solicitation Year:
2008
Solicitation Topic Code:
AF08-BT09
Solicitation Number:
2008.B
Small Business Information
Alameda Applied Sciences Corporation
3077 Teagarden St. San Leandro, CA 94577-5720
View profile »
Woman-Owned: No
Minority-Owned: Yes
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2011
Title: Variable Thrust/Specific Impulse Electrospray Propulsion
Agency / Branch: DOD / USAF
Contract: FA9550-11-C-0027
Award Amount: $750,000.00
 

Abstract:

ABSTRACT: Future Department of Defense space missions require precise, fine-positioning capabilities combined with large maneuvrability requirements. The purpose of this STTR is to: a) identify propellants for electrospray propulsion able to cover, at high propulsion efficiency, an unusually wide range of specific impulses, from several hundred seconds, typical today of colloidal propulsion up to values of thousands of seconds, typical today of only purely ionic propulsion; and b) meet thrust requirements by microfabricated multiplexed electrosprays. The challenge will be met with a fixed thruster and propellant. No electrostatic ion thruster based on ions of fixed mass/charge is suitable to span such a wide specific impulse range at high propulsion efficiency and full power. Electrospray propulsion, on the other hand, has this useful characteristic, since it admits a wide range of mass/charge values at relatively constant beam power. One can therefore use the full power available over the whole range of specific impulse with a single propellant. This STTR collaboration aims to validate this exciting new approach to micro-electric propulsion for military and civilian nano-satellite applications, capitalizing on the unique combination of expertise of the Yale-AASC team. BENEFIT: This project will develop innovative, on orbit propulsion methods that provide variable high thrust and high specific impulse at high efficiency, and enable system orbit agility or new orbit regimes. The high efficiency over an unprecedented range of specific impulse makes the electrospray micro-thruster a key enabling technology for all future nano-satellites.

Principal Investigator:

Mahadevan Krishnan
President
(510) 483-4156
krishnan@aasc.net

Business Contact:

Mahadevan Krishnan
President
(510) 483-4156
krishnan@aasc.net
Small Business Information at Submission:

Alameda Applied Sciences Corporation
3077 Teagarden Street San Leandro, CA 94577-

EIN/Tax ID: 943201700
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: Yes
HUBZone-Owned: No
Research Institution Information:
Yale University
Grant/Contract Administration
155 Whitney Avenue, suite 214
New Haven 06520 8337, CT 06520-
Contact: Nadira Clarke
Contact Phone: (203) 432-2460