SBIR/STTR Research Award

Advanced Vortex Hybrid Propulsion System (AVHPS)

Award identifier b02a753ff46af373bf25d81b29abea647340afcc4e138f542fd39c5823b012e1Awarding agency Department of Defense · Air Force

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

2003

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Orbital Technologies Corporation
Proposal award date
Not reported
Contract end date
Not reported
UEI
XESXD6N437K9
Solicitation number
Not reported
Topic code
Not reported

Research abstract

ORBITEC proposes to develop an Advanced Vortex Hybrid Propulsion System (AVHPS) to meet the demands of highly-reliable, low-cost propulsion systems for small launch vehicles. The benefits of the AVHPS result from the combination of ORBITEC's patentedvortex injection technique and high-regression rate solid fuels. The AVHPS will provide for high volumetric loading and energy density, high combustion efficiency, reliable system performance, safe storage and deployment, and low cost. The Phase I workincludes launch vehicle conceptual designs and trade studies, modifications to an existing thrust chamber assembly, fuel burning characterization under the vortex combustion scheme, throttling and mixture ratio control tests, empirical regression rate andcombustion efficiency correlation development, technical risk identification and management, and Phase II thrust chamber design and test plan. This technology aims to improve propulsion system performance, reliability, and reduce costs associated withsmall launch vehicle propulsion systems. The end product of the overall research and development program will also have application to sounding rockets, reusable and expendable launch vehicles, and upper stage propulsion systems for orbit-insertion.Near-term military applications include: boost-phase interceptors, high-speed and/or high altitude target drones, cruise missile propulsion, and forward observation craft propulsion. Military orbit transfer propulsion systems and satellite maneuveringpropulsion systems can also benefit from this technology. This technology is closely related to ORBITEC's vortex combustion cold-wall (VCCW) chamber technology for liquid bi-propellant applications, and has the potential to dramatically improve liquidrocket and RBCC lifetime, reusability, and thrust-to-weight ratio. Future generation launch vehicles can benefit from these technologies. In addition to these applications, this new type of vortex combustion may have significant industrial benefits. Forexample, many classes of air-fired combustors can use the vortex combustion technology for improved combustion efficiency and potentially reduced emissions.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

216 SBIR/STTR records share this UEI (1989–2014). Reported award amounts total $56,646,148. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense, Department of Agriculture, Department of Health and Human Services, National Science Foundation, Department of Energy

Agency intelligence

Department of Defense

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