Advanced Reusable Launch Vehicle (RLV) Systems Technology Qualis Corporation Huntsville, AL

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Advanced Reusable Launch Vehicle (RLV) Systems Technology Qualis Corporation Huntsville, AL Innovation Defined the techniques and model hardware innovations for a new class of short duration base heating tests that are an order of magnitude cheaper to develop and operate than previous tests of this type. Accomplishments A 2.25% scale model of the X-33 flight demonstrator has been successfully hot fired. The model simulates the propulsion system hot exhaust gases for the X-33, and provides data which are useful in quantifying and validating the thermal environment in the aft end of the vehicle during powered flight. Nitrogen buffer gas delivery system and fast acting electrically actuated propellant valve capability has been demonstrated. Commercialization The hardware and testing method will be marketed to Launch Vehicle prime contractors to support their development of the RLV, Expendable Launch Vehicles and Air Breathing Reusable Launch Vehicles. A simplified set of test hardware will be offered along with the instructional software as a teaching aid and research tool for mechanical, Government/Science Applications X-33 Plume induced convective heating and base pressure environment definition. Potential application to RLV and future launch vehicles. A Phase III contract will assist in conducting X-33 high altitude testing in MSFC Nozzle Test Facility. Phase II was up to 10X cheaper than STS Test. X-33 Model Plume High Speed Film Points of Contact: - NASA (Denise Swain; 256/544-8112) - Qualis Corp. (Elizabeth Blackwood; 256/533-9282) 1995 SBIR Phase 2; NAS8-97020 Marshall Space Flight Center Date of Update: 12/10/98 Success Story #: 8-028 X-33 Base Model with Oil Flow Visualization

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Page 1: Advanced Reusable Launch Vehicle (RLV)  Systems Technology  Qualis Corporation Huntsville, AL

Advanced Reusable Launch Vehicle (RLV) Systems Technology

Qualis CorporationHuntsville, AL

Innovation Defined the techniques and model hardware innovations for a new

class of short duration base heating tests that are an order of magnitude cheaper to develop and operate than previous tests of this

type.

Accomplishments A 2.25% scale model of the X-33 flight demonstrator has been

successfully hot fired. The model simulates the propulsion system hot exhaust gases for the X-33, and provides data which are useful in quantifying and validating the thermal environment in the aft end of the vehicle during powered flight.

Nitrogen buffer gas delivery system and fast acting electrically actuated propellant valve capability has been demonstrated.

Commercialization The hardware and testing method will be marketed to Launch

Vehicle prime contractors to support their development of the RLV, Expendable Launch Vehicles and Air Breathing Reusable Launch Vehicles.

A simplified set of test hardware will be offered along with the instructional software as a teaching aid and research tool for mechanical, aerospace, and propulsion departments at Universities.

Government/Science Applications X-33 Plume induced convective heating and base

pressure environment definition.

Potential application to RLV and future launch vehicles.

A Phase III contract will assist in conducting X-33 high altitude testing in MSFC Nozzle Test Facility.

Phase II was up to 10X cheaper than STS Test.

X-33 Model Plume High Speed Film

Points of Contact: - NASA (Denise Swain; 256/544-8112) - Qualis Corp. (Elizabeth Blackwood; 256/533-9282)1995 SBIR Phase 2; NAS8-97020

Marshall Space Flight CenterDate of Update: 12/10/98

Success Story #: 8-028

X-33 Base Model with Oil Flow Visualization