oxygen propellant

oxygen propellant

[′äk·sə·jən prə′pel·ənt]
(materials)
A propellant having a minimum assay by volume of 99.9% oxygen when gasified.
References in periodicals archive ?
After launching, the BFR booster would return to the launching pad; the spaceship would continue to orbit, where it would refill its tanks of methane and oxygen propellant before embarking on the monthslong journey to Mars.
To date, the best exhaust velocity achieved with chemical engines is 4,440 meters per second using hydrogen and oxygen propellant.
The liquid oxygen propellant would require additional tanks, insulation, and thermal controls.
The RL10B-2 delivers 24,750 pounds of thrust to power the Delta IV upper stage, using cryogenic liquid hydrogen and liquid oxygen propellants.
The RL10C-1 delivers 22,890 pounds of thrust to power the Atlas V upper stage, using cryogenic liquid hydrogen and liquid oxygen propellants during its operation.
The RL10C-1 engine delivers 22,890 pounds of thrust to power the upper stage, using cryogenic liquid hydrogen and liquid oxygen propellants during its operation.
The sensors performed normally on Thursday during and after the three hours it took to fill the shuttle's external fuel tank with 500,000 pounds of liquid hydrogen and liquid oxygen propellants, according to The New York Times.
The second, or upper stage, will consist of a J-2X main engine fueled by liquid hydrogen and liquid oxygen propellants.
After the upper stage separated from the launch vehicle, a single RL10B-2 engine ignited to provide 24,750 pounds of thrust to power the upper stage, using cryogenic liquid hydrogen and liquid oxygen propellants during its operation.
The venerable RL10A-4-2 engine delivers 22,300 pounds of thrust to power the upper stage, using cryogenic liquid hydrogen and liquid oxygen propellants during its operation.
After the upper-stage separated from the launch vehicle, a single RL10B-2 engine ignited to provide 24,750 pounds of thrust to power the upper-stage, using cryogenic liquid hydrogen and liquid oxygen propellants during its operation.
The RL10C-1 engine delivers 22,890 pounds of thrust to power the Atlas V upper stage, using cryogenic liquid hydrogen and liquid oxygen propellants during its operation.