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Wavelength-Agile Optical Rocket Propulsion Sensor (WORPS)

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNS04AA99C
Agency Tracking Number: 020068
Amount: $500,000.00
Phase: Phase II
Program: STTR
Solicitation Topic Code: N/A
Solicitation Number: N/A
Solicitation Year: N/A
Award Year: 2004
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
1212 Fourier Drive, Madison, WI, 53717
DUNS: 196894869
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Martin Chiaverini
 Principal Investigator
 (608) 827-5000
Business Contact
 Eric Rice
Title: President & CEO
Phone: (608) 827-5000
Research Institution
 University of Wisconsin - Madison
 Cheri Gest
 1415 Engineering Drive
Madison, WI, 53706
 (608) 262-0252
 Nonprofit college or university
ORBITEC and the University of Wisconsin-Madison propose to continue the development of a low-cost, non-intrusive, wavelength-agile optical rocket propulsion sensor (WORPS) to interrogate rocket exhaust plumes and cryogenic fluid properties. The innovative sensor system uses an amplified Chirped White Pulse Emitter (CWPE) to generate high-power wavelength-agile light for probing rocket plumes. It also uses a high-power wavelength-multiplexed differential absorption scheme for probing LOX lines. The plume sensor provides planar images of gas temperature and species concentrations. Furthermore, these measurements will be continuous (one planar measurement every 62 ?Ys) and therefore useful for monitoring the evolution of rocket plume properties. The LOX portion of the Phase II system will be capable of accurate (better than 0.1% error) measurements of LOX concentration in cryogenic fluids with 3 ?Ys time response. The LOX sensor may also be extended to enable determination of LOX flow rates. Phase II will begin with a focus on additional testing of the Phase I sensors. The sensors will then be refined, tested extensively in a variety of rocket exhaust plumes and in a LOX delivery system, and assembled into a portable, user-friendly package for delivery to NASA/SSC.

* Information listed above is at the time of submission. *

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