NASA SBIR 2015 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 15-1 H2.01-8819
SUBTOPIC TITLE: In-Space Chemical Propulsion
PROPOSAL TITLE: ORSC Methane Ascent/Descent Engine Technology Development

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Special Aerospace Services
3005 30th Street
Boulder, CO 80301 - 1304
(303) 625-1010

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Tim Bulk
tbulk@specialaerospaceservices.com
3005 30th Street
Boulder, CO 80301 - 1304
(303) 625-1010

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Kimberley Lopez
khutto@specialaerospaceservices.com
3005 30th Street
Boulder, CO 80301 - 1304
(303) 747-6885

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 4

Technology Available (TAV) Subtopics
In-Space Chemical Propulsion is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Special Aerospace Services (SAS) is proposing a new and innovative ascent/descent engine using methane as its propellant. This engine will utilize the concepts of the Oxidizer Rich Staged Combustion (ORSC) cycle of the RD-8 to improve on performance over existing hardware. This SBIR program will leverage existing work SAS has done in conjunction with DARPA to on the RD-8 preburner to design and analyze a new engine with the benefits of the RD-8, but being able to use methane as the propellant. Additive manufacturing will be used to build the components of the engine to reduce cost and limitations in design.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
NASA has the opportunity to support the development of an ascent/descent methane engine for use in exploration missions that will greatly expand the capability for the agency. Opportunities for NASA include small autonomous and rendezvous space tug engine for orbital debris removal, Mars sample ascent and descent engine, micro-lander applications, and other interplanetary missions.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Non-NASA applications include research by DARPA and other government agencies such as the U.S. Air Force. Interests may include providing an upper stage for Super Strypi, or as an application with DARPA's ALASA program. Additional Non-NASA commercial applications include micro-lander applications, orbit debris removal systems, and exploratory interplanetary missions.

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Cryogenic/Fluid Systems
Fuels/Propellants
Heat Exchange
Metallics
Prototyping
Simulation & Modeling
Space Transportation & Safety
Spacecraft Main Engine

Form Generated on 04-23-15 15:37