EVALUATION OF AN AUGMENTED SPARK IGNITER'S FLAME LENGTH, COMPARISON OF NUMERICAL, EXPERIMENTAL INVESTIGATIONS
|
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
|
2019 |
Herrera, Manuel |
OPTIMIZATION OF REGENERATIVELY COOLED ROCKET ENGINES COOLING CHANNEL DIMENSIONS
|
2019 |
Atefi, Ehsan |
DEVELOPMENT STATUS OF LE-9 ENGINE FOR H3 LAUNCH VEHICLE
|
2019 |
Kawashima, Hideto |
PRELIMINARY RESULTS OF A MICROPUMP FOR MON-25/MMH PROPULSION, ATTITUDE CONTROL
|
2019 |
Besnard, Andrea |
SMALL-SCALE HYDROGEN PEROXIDE VAPOR PROPULSION SYSTEM: CATALYST PERFORMANCE, HEAT TRANSFER
|
2019 |
Rhodes, Brandie L. |
CONJUGATED COMBUSTION, HEAT TRANSFER SIMULATIONS OF UPPER, LOWER MAIN COMBUSTION CHAMBERS OF LE-9 ENGINE
|
2019 |
Daimon, Yu |
INVESTIGATION OF THE EFFECT OF GEOMETRICAL PARAMETERS OF PRESSURE SWIRL ATOMIZER ON THE HOLLOW CONE SPRAY
|
2019 |
Tokgöz, Tolga |
FINAL DAWN REACTION CONTROL SYSTEM (RCS) PROPULSION SYSTEM IN-FLIGHT CHARACTERIZATION
|
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 |
DESIGN, FABRICATION, TEST, LAUNCH,, EARLY OPERATION OF THE PARKER SOLAR PROBE PROPULSION SYSTEM
|
2019 |
Kijewski, Seth |
LIQUID ROCKET ENGINE TORCH IGNITER FEED SYSTEM
|
2019 |
Vadera, Atticus J. |
UPDATE ON THE STUDENT DEVELOPMENT OF A NITROUS OXIDE-ETHANE BIPROPELLANT ROCKET ENGINE
|
2019 |
Perry, McKynzie |
NUMERICAL INVESTIGATION OF BULK VELOCITY, PRESSURE ON NEAR WALL CHEMISTRY IN FUEL RICH RP-2/GOX COMBUSTION
|
2019 |
Kulakhmetov, Rufat F. |
A FIRST STEP INTO THE BLANCHING MODELLING OF LIQUID ROCKET ENGINES: TAKING INTO ACCOUNT THE ROUGHNESS INCREASE OF THE CHAMBER WALL
|
2019 |
Riccius, Jöerg R. |