SBIR/STTR Research Award

High Duty Cycle, Extended Operation Constant Volume Combustion Engine

Award identifier 76d22c784380dd1d0604577aaf1ee0e2dc9071d388d3f16c625bd2f3d2b33575Awarding agency National Aeronautics and Space Administration

Award amount

$96,337

Program and phase

SBIR · Phase I

Award year

2011

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
STREAMLINE AUTOMATION LLC
Proposal award date
2011-02-18
Contract end date
2011-09-29
UEI
CLW2B8WVV1D4
Solicitation number
Not reported
Topic code
S3.04

Research abstract

The Science Mission Directorate is chartered with answering fundamental questions requiring the view from and into space. Its future direction will be moving away from exploratory missions (orbiters and flybys) into more detailed/specific exploration missions that are at or near the surface of planets and small bodies (landers, rovers, and sample returns) or at more optimal observation points in space. This drives a need for propulsion technologies that enable precision landing, hazard avoidance, in-space rendezvous, and ascent/decent vehicle propulsion. These missions will entail higher propulsion system duty cycles, more challenging environmental conditions, and extended operation. Moreover, propulsion system objectives will need to be met with more stringent constraints on mass, volume, power, and cost.C3 Propulsion proposes the development of an advanced CV engine prototype featuring an innovative combination of multiple throttling techniques to enable sustained deep throttling without sacrificing engine performance. The Constant Volume combustion engine is an innovative design that combines light weight, low pressure fuel tanks and operates at high chamber pressures. The CV engine has nearly identical specific impulse as a constant pressure engine with the same mass flow and throat area, furthermore, the nozzle optimizes at the same area ratio. It has exceptional thrust-to-weight ratios.It will be designed for high duty cycle, extended operation to satisfy SMD mission requirements. The suitability of this engine for a range of SMD missions will be proven through engine testing that demonstrates deep throttling capability, and the development of appropriate scaling laws that allowengine sizing to be performed based on mission requirements.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

75 SBIR/STTR records share this UEI (2003–2024). Reported award amounts total $23,124,794. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

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

Agency intelligence

National Aeronautics and Space Administration

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