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Carbon aerogel thermal protection system for reusable launch vehicles
Ceramic matrix composite material in highly loaded journal bearings
CFD Analysis in the Design of a Water-Jet-Drive System
CFD Analysis of Modular Thrusters Performance
CFD Analysis of the 24-Inch Jirad Hybrid Rocket Motor
CFD Analysis of the ATD HPFTP Inlet Guide Vanes
CFD Flow Analysis and Code Validation for the MSFC Eight-Percent ASRM Cold Flow Model Part II
CMC/METALLIC TECHNOLOGY FOR THE REUSABLE SPACE RIDER BODY FLAP ASSEMBLY
Combined satellite systems for continuous global coverage in equatorial and polar circular orbits
COMBUSTION OF ALUMINIZED SOLID PROPELLANTS WITH BIMODAL OXIDIZER PARTICLE SIZE DISTRIBUTION
Combustion Processes in Hybrid Rocket Engines
Combustion Zone Characterization of GO~2/GH~2 Rocket Using Laser-Induced Fluorescence of OH
Combustor Modeling Under Gox-Rich Conditions
COMPARATIVE ANALYSIS OF UPPER STAGE AND BUILT-IN PROPULSION SYSTEM FOR GEO SATELLITE LAUNCHES
COMPLEX NUMERICAL SIMULATION OF THE LAUNCH SYSTEM GAS-DYNAMICS
Computational Analysis of Volutes
Computational and Experimental Efforts in Gravity Probe B Microthruster Analysis
CONCEPT DESIGN OF AN IN-ORBIT PROPULSION SYSTEM BASED ON MAGNETOFLUIDS
CONCEPTUAL DESIGN OF A NANOLAUNCHER BASED AEROSPIKE NOZZLE TO SEND CUBESATS FROM MEXICO
CONSTRUCTION TECHNOLOGY OF INTELLIGENT SPACE LAUNCH COMMAND AND CONTROL SYSTEM IN LAUNCH SITE
Control Reconfiguration on Deadlocked Gimballed Thrust of Launch Vehicle
Correlation-log-based underwater navigation
CURRENT COMMERCIAL LANDSCAPE OF SMALL SATELLITE LAUNCH SERVICES IN THE US AND EUROPE
Das deutsche Bodenstationssystem für den Funkverkehr mit Satelliten
Der deutsche Forschungssatellit und der deutsch-französische Nachrichtensatellit
DESIGN AND DEVELOPMENT OF A BRAZILIAN LIQUID ENGINE SOUNDING ROCKET TO TRAIN LAUNCH OPERATIONS
DESIGN AND DEVELOPMENT OF A BRAZILIAN LIQUID ENGINE SOUNDING ROCKET TO TRAIN LAUNCH OPERATIONS
DESIGN AND FABRICATION OF REACTION CONTROL SYSTEM FOR MODEL ROCKETS
DESIGN AND VERIFICATION OF A ROCKET'S MIRRORING SYSTEM BASED ON DIGITAL TWIN TECHNOLOGY
DESIGNING OF LANDING SYSTEM FOR MARS USING ELECTROMAGNETIC FORCE
DESIGN MODIFICATIONS FOR PERFORMANCE ENHANCEMENT OF A SUBORBITAL ROCKET ILR-33 AMBER 2K
Design of controller switching scenario for reusable launch vehicle with elevon jamming failure
Design of rockets and space launch vehicles