Design and Performance Evaluation of an Exhaust Diffuser for Altitude Testing of Chemical Rocket Engines
Author:
Affiliation:
1. Purdue University
2. Northrop Grumman Corporation
Publisher
American Institute of Aeronautics and Astronautics
Reference12 articles.
1. Design and Analysis of a Second-Throat Exhaust Diffuser for Altitude Simulation
2. Effects of Vacuum Chamber and Reverse Flow on Supersonic Exhaust Diffuser Starting
3. Hypergolic Ignition of a Paraffin-Based Hybrid Motor with MON-25 at 100,000 ft Simulated Altitude
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1. Performance Evaluation of a Diffuser –Ejector System using Cold Gas Thrusters with Different Nozzle Geometries in the Purdue Altitude Chamber Facility;AIAA SCITECH 2023 Forum;2023-01-19
2. Numerical & Experimental Investigation of a Diffuser –Ejector System Performance using Cold Gas Thrusters with Conical & Thrust Optimized Bell Nozzles;AIAA Propulsion and Energy 2021 Forum;2021-07-28
3. A simplified design approach for high-speed wind tunnels: part II. Diffuser optimization and complete duct design;Journal of Mechanical Science and Technology;2021-06-29
4. Hypergolic Ignition of a Paraffin-Based Hybrid Motor with MON-25 at 100,000 ft Simulated Altitude;AIAA Propulsion and Energy 2020 Forum;2020-08-17
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