140457 ⎘
Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
Nozzle with Widely-Spaced Thrust Chambers, Engine Including the Nozzle, and Vehicle Including the Engine
#2ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED HEAT SHIELD
#3REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE
#4ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED BASE HEAT SHIELD
#5REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE
#6ROLL CONTROL THRUSTER AND HYBRID ROCKET COMPRISING SAME
#7Non-axisymmetric heat shield, a nozzle defined at least partially by the heat shield, an engine including the nozzle, and a vehicle including the engine
#8Annular aerospike nozzle with widely-spaced thrust chambers, engine including the annular aerospike nozzle, and vehicle including the engine
#9Ring-shaped booster rocket
#10Ring-shaped booster rocket
#11Integrated thruster
#12Device and system for controlling missiles and kill vehicles operated with gel-like fuels
#13Microfluidic homogeneous catalyzation systems and methods, and apparatuses incorporating same
#14Small satellite propulsion system
#15Deflector for a thrust flow powered vehicle and thrust flow powered vehicle with said deflector
#16Jet propulsion device and fuel supply method
#17Vectored-thrust propulsor
#18Cryogenic thruster assembly using regenerative heating from main and settling thrusters
#19Rocket nozzles for unconventional vehicles
#20Belted toroid pressure vessel and method for making the same
#21SYSTEM AND METHOD FOR MANEUVERING ROCKETS
#22Control and/or drive device for a flying body
#23Satellite Control
#24Rocket nozzles for unconventional vehicles
#25Dual-mode chemical-electric thrusters for spacecraft
#26FORCE BALANCED BUTTERFLY PROPORTIONAL HOT GAS VALVE
#27Side thruster module
#28Rocket engine having guide vanes in the nozzle of the engine
#29Control and/or drive device for a flying body
#30Fluidic diverter valve with a variable valve-bore clearance
#31Chemical and cold gas propellant systems and methods