SBIR/STTR Research Award

Spectral Measurement System for Health Monitoring of Liquid Rocket Engines

Award identifier 58a7379273a50be71a238fe9d02a50d24b1fd3e107b8ca135b413486ed13dc8bAwarding agency Department of Defense · Air Force

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

2011

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
OPTO-KNOWLEDGE SYSTEMS INC
Proposal award date
2010-12-16
Contract end date
Not reported
UEI
RJH6GQUD3BT5
Solicitation number
2009.3
Topic code
AF093-187

Research abstract

OKSI proposes to demonstrate the ability to detect metallic species in a hydrocarbon fueled liquid rocket engine (LRE) using high resolution emission spectroscopy. The detection of metallic species is an indication of engine wear and an early precursor to a catastrophic failure. During Phase-I, OKSI will conduct exhaust plume measurements of a sub-scale GOX/RP-1 rocket engine. Metallic contaminants will be added to the fuel prior to combustion. Two high resolution UV/VIS spectrometers will be fielded. A third MWIR spectrometer (which measures primary combustion products) will be fielded to assist in accurate modeling of the rocket engine. During Phase-II OKSI will conduct more extensive measurements using the same spectrometers. The measurements may be enhanced using Laser Induced Breakdown Spectroscopy (LIBS). High fidelity modeling and simulation will be performed using enhanced versions of the JANNAF engine/plume codes and other specialized signature codes. The Phase-II effort will culminate with the design, development, and demonstration of a ruggedized, high resolution spectrometer and data analysis system optimized for hydrocarbon fueled engine health monitoring. BENEFIT: The next generation military and commercial space lift systems will utilize reusable, fly-back first stage boosters to reduce cost. These systems must be quickly turned around for subsequent missions. Reliable, nonintrusive exhaust plume health monitoring is desirable to support this need. The technology developed under this project will enable the detection of metallic species, which is an indication that the engine may need maintenance. As such, the system developed under this program will have direct benefit to commercial space launch vehicles by improving the safety and reliability of the engines. The technology also has direct applications to commercial (and military) turbojet aircraft. The engine health monitoring system technology developed could be used as part of the engine check-out procedure, and once the system proves reliable, it could actually be utilized to reduce the required scheduled maintenance (downtime) for aircraft. Thus, in addition to increasing safety, an aircraft engine health monitoring system could also reduce operating costs. These abilities have the potential to prevent catastrophic failures at launch and save hundreds of millions of dollars when expensive payloads are lost. Failures also cripples the US operational ability when unique payloads are lost.

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

180 SBIR/STTR records share this UEI (1991–2025). Reported award amounts total $90,018,148. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, Department of Commerce

Agency intelligence

Department of Defense

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