FINAL DAWN REACTION CONTROL SYSTEM (RCS) PROPULSION SYSTEM IN-FLIGHT CHARACTERIZATION
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2019 |
Barber, Todd J. |
DEVELOPMENT OF A LOX/ETHANOL GAS GENERATOR FOR A HYBRID-MOTOR-BASED MINI-LAUNCHER
|
2019 |
Paccagnella, Enrico |
SUPERCRITICAL GN2/GH2 JET MODELED BY THE ECS METHOD
|
2019 |
Yao, Wei |
MODULAR LIQUID PROPELLANT LAUNCH VEHICLE DESIGN
|
2019 |
Honkawa, Derek Y. |
GENESIS, APPLICATION OF SMC-S-025: EVALUATION, TEST REQUIREMENTS FOR LIQUID ROCKET ENGINES
|
2019 |
Fusselman, Steven |
ROCKET ENGINE DIGITAL TWIN – MODELING, SIMULATION BENEFITS
|
2019 |
Mena, David Jimenez |
AMC9 Successful Reorbitation - Propulsion Challenges
|
2019 |
Kruch, Eric |
DESIGN OF THE EUROPA CLIPPER PROPELLANT MANAGEMENT DEVICE
|
2019 |
Manning, Robert E. |
UNCERTAINTY ANALYSIS OF EXPERIMENTAL DISCHARGE COEFFICIENTS IN ADDITIVELY MANUFACTURED LIQUID INJECTOR ELEMENTS
|
2019 |
Venters, James P. |
STUDENT DEVELOPMENT OF A LIQUID OXYGEN, LIQUID METHANE SOUNDING ROCKET, LAUNCH INFRASTRUCTURE
|
2019 |
Meriam, Silas |
CARBON DEPOSIT FORMATION IN SUPERCRITICAL METHANE-BASED, HYDROCARBON FUELS USING A COOLING CHANNEL SURROGATE
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2019 |
Driscoll, Robert |
COMPUTATIONAL INVESTIGATION ON THE EFFECT OF THE OXIDIZER INLET TEMPERATURE ON COMBUSTION INSTABILITY
|
2019 |
Harvazinski, Matthew E. |
SHUTDOWN INVESTIGATION IN A LOX-ETHANOL SUBSCALE THRUST CHAMBER
|
2019 |
Dias, Iago Dalmaso Brasil |
EFFECTS OF THE RECESS LENGTH ON FLOW, COMBUSTION STABILITY OF GAS-CENTERED COAXIAL SWIRL INJECTORS
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2019 |
Wang, Yuangang |
NUMERICAL TOOL OPTIMIZATION FOR ADVANCED ROCKET NOZZLE PERFORMANCE PREDICTION
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2019 |
Conte, Antonietta |
EVALUATION OF AN AUGMENTED SPARK IGNITER'S FLAME LENGTH, COMPARISON OF NUMERICAL, EXPERIMENTAL INVESTIGATIONS
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2019 |
Öz, Levent Ç. |
IMPACT OF SUPERCRITICAL, TRANSCRITICAL EFFECTS ON ROCKET ENGINE INJECTOR MASS FLUX, STIFFNESS
|
2019 |
Gloria, Nicholas |
DESIGN, TESTING OF A 500 LBF LIQUID OXYGEN/LIQUID METHANE ENGINE
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2019 |
Herrera, Manuel |
OPTIMIZATION OF REGENERATIVELY COOLED ROCKET ENGINES COOLING CHANNEL DIMENSIONS
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2019 |
Atefi, Ehsan |
DEVELOPMENT STATUS OF LE-9 ENGINE FOR H3 LAUNCH VEHICLE
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2019 |
Kawashima, Hideto |