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Ionic Liquid, Nontoxic Monopropellants for Power-Limited Spacecraft

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX12CD84P
Agency Tracking Number: 115460
Amount: $124,849.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: S3.04
Solicitation Number: N/A
Timeline
Solicitation Year: 2011
Award Year: 2012
Award Start Date (Proposal Award Date): 2012-02-13
Award End Date (Contract End Date): 2012-08-13
Small Business Information
3100 Fresh Way Southwest
Huntsville, AL 35805-3637
United States
DUNS: 124289294
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Roberto Di Salvo
 Principal Investigator
 (256) 713-1220
 roberto.disalvo@streamlineautomation.biz
Business Contact
 Aijalon Putzier
Title: Business Official
Phone: (256) 713-1220
Email: aijalon.putzier@streamlineautomation.biz
Research Institution
 Stub
Abstract

A key requirement of modern chemical energetic materials include enhanced performance, reduced sensitivities, and reduced toxicity. A class of compounds that meet these requirements is Ionic Liquids (ILs). The physicochemical properties of ILs enable their use in a variety of applications and energetic ionic liquids (EILs) is an area of intense research in the last decade.C3 Propulsion proposes the study and development of advanced ionic liquid, non-toxic monopropellants featuring an innovative combination of anions and cations that will enable high duty cycle, extended operation of power-limited spacecraft.This Phase I effort will demonstrate the feasibility of non-toxic monopropellants for power-limited spacecraft. This effort will build on a successful project that built and tested an on-demand EIL gas generator. The project will extend past work on non-toxic EIL monopropellants, test different anion/cation combinations to seeks optimization of the EIL, and conduct studies of the catalyst bed to identify the optimal distribution and modality.In Phase II, the development and optimization of the EIL monopropellant system will continue. This will include targeting improvement of the flow control valves, propellant injectors, and thrust chamber catalyst bed design for use with the selected low toxicity monopropellant. Programmatically, there will be an aggressive push towards flight-like hardware to ensure rapid maturation of the technology in order to meet the NASA mission goals.

* Information listed above is at the time of submission. *

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