Nitrous Ethane-Ethylene Rocket with Hypergolic Ignition

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX15CC61P
Agency Tracking Number: 154841
Amount: $124,881.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: S3.02
Solicitation Number: N/A
Timeline
Solicitation Year: 2015
Award Year: 2015
Award Start Date (Proposal Award Date): 2015-06-17
Award End Date (Contract End Date): 2015-12-17
Small Business Information
11111 West 8th Avenue, Unit A, Lakewood, CO, 80215-5516
DUNS: 120561456
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Robert Zubrin
 Principal Investigator
 (303) 980-0890
 zubrin@aol.com
Business Contact
 Robert Zubrin
Title: Business Official
Phone: (303) 980-0890
Email: zubrin@aol.com
Research Institution
N/A
Abstract
The Nitrous Ethane-Ethylene Rocket with Hypergolic Ignition (NEERHI) engine is a proposed technology designed to provide small spacecraft with non-toxic, non-cryogenic, high performance, hypergolic propulsion. When passed over a warm ruthenium catalyst bed, gaseous nitrous oxide and an ethylene-ethane gaseous blend combust instantly. A small 1 N thruster can be designed to provide small satellite propulsion systems with a specific impulse of approximately 300 seconds. Both propellants are self-pressurizing, capable of delivering feed line pressures in excess of 800 psi at room temperature, and 400 psi if cooled to 0?C. For longer duration missions, both nitrous oxide and an ethane-ethylene fuel blend do not require thermal heating to maintain a liquid state, and as such, can be stored on Earth or in space for in-definite periods of time with no parasitic power drain required to maintain a liquid propellant. Compared to other available chemical propulsion systems, a NEERHI system offers a cost effective solution as other hypergolic engines use hydrazine and nitrogen tetroxide which are toxic and dangerous to handle, increasing ground costs. As an added capability, the NEERHI engine has the ability to operate as a monopropellant engine if the ruthenium catalyst be is heated with a bipropellant reaction, increasing the lifetime of the catalyst bed and reducing heating loads on the engine.

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

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