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Altitude Compensating Nozzle Transonic Performance Flight Demonstration

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
67342
Program Year/Program:
2004 / SBIR
Agency Tracking Number:
035782
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
K T Engineering Corporation
238 Business Park Boulevard, Building 23B Suite J Madison, AL 35758-7552
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Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 2004
Title: Altitude Compensating Nozzle Transonic Performance Flight Demonstration
Agency: NASA
Contract: NND04AA48C
Award Amount: $69,920.00
 

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.

Principal Investigator:

Richard Denton
Principal Investigator
2564895832
dick.denton@kte-aerospace.com

Business Contact:

David Sisk
Business Official
2564895832
david.sisk@kte-aerospace.com
Small Business Information at Submission:

K T Engineering Corporation
4835 University Square, Suite 2 Huntsville, AL 35816

EIN/Tax ID: 010707745
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No