NASA SBIR 2012 Solicitation


PROPOSAL NUMBER: 12-1 E1.02-9215
SUBTOPIC TITLE: Nano/Micro Satellite Launch Vehicle Technology
PROPOSAL TITLE: Regeneratively-Cooled, Pump-Fed Propulsion Technology for Nano / Micro Satellite Launch Vehicles

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Ventions, LLC
1142 Howard Street
San Francisco, CA 94103 - 3914
(415) 543-2800

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Adam P London
1142 Howard Street
San Francisco, CA 94103 - 3914
(415) 543-2800

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Amit Mehra
1142 Howard Street
San Francisco, CA 94103 - 3914
(202) 213-2846

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 4
End: 5

Technology Available (TAV) Subtopics
Nano/Micro Satellite Launch Vehicle Technology is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Ventions proposes the development of a pump-fed, 2-stage nano launch vehicle for low-cost on demand placement of cube and nano-satellites into LEO. The proposed vehicle uses high T/W and Isp pump-fed engines that operate at chamber pressures >750psi without the weight penalty of high pressure tanks, thereby realizing payload fractions in the 1-2% range. Ventions has already completed several component-level demonstrations in the area, and is proposing additional optimization / testing of a 5,000lbf LOX / RP-1 turbopump-fed engine as part of this Phase I in-order to demonstrate a flight-ready 1st stage propulsion system.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed nano launch vehicle is aimed at providing low-cost and on-demand insertion of NASA cube- and nano-satellites into LEO as primary payloads. This will change the current model of launching such satellites as secondary payloads (which are often constrained by requirements of
the primary payload), thereby extending this capability to a wider range of NASA experimental missions requiring on-demand and low-cost insertion of small sattelites into specific orbits.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Non-NASA applications for the same will include DoD and military missions requiring rapid on demand access to space from anywhere in the world (based on ground or air-launch), as well as university and research satellites. Additionally, the small-scale thrust chamber assemblies and turbomachinery technology components developed for the launch vehicle are also expected to have widespread applications in other in-space propulsion systems, upper stages, and orbital insertion / maneuvering thrusters, etc.

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
Launch Engine/Booster
Spacecraft Design, Construction, Testing, & Performance (see also Engineering; Testing & Evaluation)
Spacecraft Main Engine
Vehicles (see also Autonomous Systems)

Form Generated on 03-28-13 15:21