NASA SBIR 2004 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 04-II X6.01-7813
PHASE-I CONTRACT NUMBER: NNM05AA50C
SUBTOPIC TITLE: Earth-to-Orbit Propulsion
PROPOSAL TITLE: Advanced Vortex Hybrid Rocket Engine (AVHRE)

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Orbital Technologies Corporation
Space Center, 1212 Fourier Drive
Madison ,WI 53717 - 1961
(608) 827 - 5000

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Ronald R. Teeter
koffarnusl@orbitec.com
1212 Fourier Drive
Madison, WI  53717 -1961
(608) 827 - 5000

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
ORBITEC proposes to develop a unique Advanced Vortex Hybrid Rocket Engine (AVHRE) to achieve a safe, highly-reliable, low-cost and uniquely versatile propulsion system. The benefits of AVHRE result from the combination of four innovations: (1) the patented vortex injection technique which generates a coaxial vortex pair, driving high solid-fuel regression rates and improved combustion efficiency; (2) high-regression rate paraffin solid fuels; (3) patented regression sensor technology, and (4) a new fuel formulation innovation to control the solid fuel regression characteristics and provide improved structural integrity of the grain. These innovations simplify hybrid rocket design, development, and manufacture both inherently and by providing many practical design degrees of freedom that can be harnessed for a given application. Specific benefits of the AVHRE technology include: (1) increased propellant mass fractions; (2) the ability to tailor and optimize a hybrid propulsion system for a given application; (3) increased ISP efficiency; (4) a reduction or elimination of residual fuel; (5) improved grain structural integrity and increased thermal properties; and (6) reduced need for thermal insulation. The Phase II effort will design, develop, and test a 10,000 lbf AVHRE-I chamber and a suite of practical AVHRE engineering design tools that will be delivered to NASA upon completion of the project.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The AVHRE addresses key design, performance, and operational challenges of traditional hybrid rocket engine systems. If successful, this would catapult hybrid rocket systems into a highly competitive position for many Earth-to-orbit propulsion applications, where their inherent safety, simplicity, and low-cost could be competitively harnessed. The AVHRE hardware, analysis, and engineering design approaches developed during the Phase II program will be useful tools that NASA will benefit from. AVHRE addresses the need for high performance, low cost, reliable/safe, and flexible propulsion technology required for Earth-to-Orbit (ETO) applications and planetary missions. The fuel formulation technology demonstrated during the Phase I AVHRE project can also likely be adapted for producing ISRU fuel grains to meet Martian and Lunar propulsion needs.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
AVHRE is expected to have a competitive position in reusable and expendable launch vehicles, sounding rockets, and upper stage propulsion systems. A new market is also emerging to provide suborbital launch vehicles for space tourists. The AVHRE could play a vital role due to its inherent safety and lower development cost. ORBITEC is also closely investigating the entertainment markets, including rocket car demonstrations at air shows, amusement rides, and model rocketry packages that would use the cartridge loaded AVHRE propulsion system. In addition to these applications, this new type of vortex combustion may have significant industrial benefits. For example, many classes of air-fired combustors can use the vortex combustion technology for improved combustion efficiency, potentially reduced emissions, and to reduce the required pre-processing.


Form Printed on 08-01-05 13:52