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Material Property Sensitivities on Cryo Upperstage Rocket Engines
Flight Test Results of the F-16 Aircraft Modified with Axisymmetric Vectoring Exhaust Nozzle
Nozzle Exit Exhaust Products from Space Shuttle Boost Vehicle (November 1973 Design)
Development of Low Cost Ablative Nozzles for Large Solid Propellant Rocket Motors
Evaluation of Dual Flow Thrust Vector Nozzles with Exhaust Stream Impingement
Recruit Nozzle Alignment Analysis to Minimize Thrust Misalignment
Radiometric Analysis from the 26-kW Electric Propulsion Space Experiment (ESEX) Flight
Aerodynamics of 3-D Aircraft Afterbodies (L'Aerodynamique des Arriere-corps Tridimensionnels)
1999 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 1
'Wake Steering' - A New Approach to Propulsion and Control
Experimental Investigation of Outflow of a Boiling Liquid Through a Centrifugal Injector Nozzle
Exploring in Aerospace Rocketry. 7 - Liquid Propellant Rocket Systems
Research and Development of Advanced Propulsion Systems Study (U)
F-15 8.33-Percent Model Internozzle Dynamic Pressure Environment
Study of Flow of Partially Ionized Argon in Hypersonic Nozzles
An Evaluation of Direct Current Electromagnetic Propulsion in Seawater
Scramjet Nozzle Design and Analysis as Applied to a Highly Integrated Hypersonic Research Airplane
Scramjet Nozzle Design and Analysis as Applied to a Highly Integrated Hypersonic Research Airplane
Development and Test of an Automatic-Shutoff Closed-Circuit Refueling System for the UH-1 Helicopter
System for Controlling the Nozzle Throat Area of a Rocket Motor
Helicopter Icing Spray System (HISS) Nozzle Improvement Evaluation
Experimental Study of Aeroelastic Instability of Overexpanded Rocket Nozzle Extensions
JANNAF Propulsion Meeting Held in Indianapolis, Indiana on February 24 - 27, 1992. Volume 1
Cart3D Analysis of Plume and Shock Interaction Effects on Sonic Boom
Low Cost Servo Actuator for Tactical Missile Thrust Vector Control (TVC)