bipropellant उदाहरण वाक्य
उदाहरण वाक्य
- For example, a mixture ratio of a bipropellant could be adjusted such that it may not have the optimal specific impulse, but will result in fuel tanks of equal size.
- Larger satellites usually use monopropellants or bipropellant combustion systems for propulsion and attitude control; these systems are complex and require a minimal amount of volume to surface area to dissipate heat.
- The bipropellant system had a total capability of about 1, 900 m / s with about 550 m / s required for lunar insertion and 540 m / s for lunar departure.
- While noticeably less than the " I " sp available from hydrazine thrusters ( monopropellant or bipropellant with dinitrogen tetroxide ), the decreased toxicity makes nitrous oxide an option worth investigating.
- Apogee kick motors often employ either a bipropellant engine, with a solid fuel and a liquid oxidiser, or a monopropellant engine with both the fuel and the oxidiser in a solid state.
- In 1981, the Naval Weapons Center tried a 350 round / minute cyclic bipropellant gun, using 90 % nitric acid and a proprietary hydrocarbon ( probably a low molecular weight alkane, like propane ).
- Its main engine, which is a derivative of the system used on India's communications satellites, uses the bipropellant combination monomethylhydrazine and dinitrogen tetroxide to achieve the thrust necessary for escape velocity from Earth.
- Performance of electrothermal systems in terms of specific impulse ( Isp ) is somewhat modest ( 500 to ~ 1000 seconds ), but exceeds that of cold gas thrusters, monopropellant rockets, and even most bipropellant rockets.
- The "'Walter HWK 109-509 "'was a bipropellant rocket engine that powered the Messerschmitt Me 163 Komet and Bachem Ba 349 aircraft . It was produced by Hellmuth Walter Kommanditgesellschaft ( HWK ) commencing in 1943.
- The installed Pintle Injector, unique to TRW designed liquid propulsion systems, provides improved reliability and less costly method of fuel-oxidizer impingement in the thrust chamber than conventional coaxial distributed-element injectors typically used on liquid bipropellant rocket engines.