Synonymer & Information om | Engelska ordet BIPROPELLANT

Exempel på hur man kan använda BIPROPELLANT i en mening

• Dual mode propulsion systems combine the high efficiency of bipropellant rockets with the reliability and simplicity of monopropellant rockets.
• A tripropellant rocket is a rocket that uses three propellants, as opposed to the more common bipropellant rocket or monopropellant rocket designs, which use two or one propellants, respectively.
• A-0, a 1943 Pre-production model of the German Walter HWK 509 liquid-fuel bipropellant rocket engine.
• Dinitrogen tetroxide is a powerful oxidizer that is hypergolic (spontaneously reacts) upon contact with various forms of hydrazine, which has made the pair a common bipropellant for rockets.
• The gravitational assist from the flyby coupled with a 7 minute burn of the bipropellant rocket put Nozomi into an escape trajectory towards Mars.
• The missile used a hypergolic bipropellant combination of unsymmetrical dimethylhydrazine (UDMH) fuel in combination with red fuming nitric acid (RFNA) oxidiser.
• Both use bipropellant, namely monomethylhydrazine (MMH) as fuel and mixed oxides of nitrogen (MON3) as oxidizer.
• When used with a suitable catalyst, HTP can be used as a monopropellant, or with a separate fuel as a bipropellant.
• The R-36 is a two-stage rocket powered by a liquid bipropellant, with UDMH as fuel and nitrogen tetroxide as an oxidizer.
• The major manufacturer of German rocket engines for military use, the HWK firm, manufactured the RLM-numbered 109-500-designation series of rocket engine systems, and either used hydrogen peroxide as a monopropellant for Starthilfe rocket-propulsive assisted takeoff needs; or as a form of thrust for MCLOS-guided air-sea glide bombs; and used in a bipropellant combination of the same oxidizer with a fuel mixture of hydrazine hydrate and methyl alcohol for rocket engine systems intended for manned combat aircraft propulsion purposes.
• MXP-351 was Masten Space's internal name for a self-igniting bipropellant combination invented to fuel its small lunar landers.
• Performance of electrothermal systems in terms of specific impulse (Isp) is 500 to ~1000 seconds, but exceeds that of cold gas thrusters, monopropellant rockets, and even most bipropellant rockets.
• Hydrazine-fuelled monopropellant thrusters are used for stationkeeping, with an IHI BT-4 bipropellant engine used for insertion into geostationary orbit.
• After separating from the second stage, the Rocket Lab's Photon kick stage lifted the orbital apogee into a lunar-transfer orbit over six days by firing the HyperCurie bipropellant engine at perigee six times followed by the trans-lunar injection (TLI) burn, after which the CAPSTONE spacecraft was deployed on its journey to the Moon.

Förberedelsen av sidan tog: 325,55 ms.