Altitude Compensating Nozzle Transonic Performance Flight Demonstration

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NND04AA48C
Agency Tracking Number: 035782
Amount: $69,920.00
Phase: Phase I
Program: SBIR
Awards Year: 2004
Solicitation Year: 2003
Solicitation Topic Code: A7.02
Solicitation Number: N/A
Small Business Information
4835 University Square, Suite 2, Huntsville, AL, 35816-1845
DUNS: 127963515
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Richard Denton
 Principal Investigator
 (256) 489-5832
 dick.denton@kte-aerospace.com
Business Contact
 David Sisk
Title: Business Official
Phone: (256) 489-5832
Email: david.sisk@kte-aerospace.com
Research Institution
N/A
Abstract
Altitude compensating nozzles continue to be of interest for use on future launch vehicle boosters and upper stages because of their higher mission average Isp and superior packaging efficiency compared with conventional bell nozzle designs. The plume physics and performance of altitude compensating nozzles have been characterized through extensive cold gas wind tunnel testing, limited hot gas testing, and computational fluid dynamic modeling. However, no altitude compensating nozzle has ever been validated in flight. Questions remain regarding performance through the critical transonic regime (Mach 0.6-1.5) where a high degree of interaction is expected between the external flow around the vehicle and the hot gas plume. A Phase I study is proposed to establish feasibility of validating transonic performance for an altitude compensating nozzle using the NASA F15B Propulsion Flight Test Fixture. Under this Phase I program we will derive requirements for the test, develop preliminary designs for the flight test article, establish test plans and procedures, coordinate closely with the NASA Dryden Flight Research Center to assure experiment safety and seamless integration with the F15B/PFTF, finalize plans for Phase II, and document our results. Test article fabrication, integration, and testing will be performed during a subsequent Phase II effort.

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

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