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- W3022632962 abstract "This chapter discusses propulsion of a rocket in outer space. The thrust or specific impulse is measured by the total impulse delivered by the engine per unit weight of propellant consumed. Electric propulsion systems have also been looked into. Jhan (1968) defines electric propulsion as the acceleration of gases for propulsion by electric heating and/or by electric and magnetic body forces. Thus electro-thermal, electrostatic, and electromagnetic propulsion devices can be considered for propulsion in space. Electro-thermal devices like arcjets are popular and find space in the study. Propellants for arcjets include hydrazine (N2H4), ammonia (NH3), and hydrogen (H2). An arcjet using ammonia as the propellant produced a thrust of 2N at a specific impulse of 800 s. One-dimensional electrostatic thruster, ion stream speeds are also discussed. Hall thrusters are also studied. Under electromagnetic propulsion devices, the magneto-plasma-dynamic accelerator (MPD) is discussed in details." @default.
- W3022632962 created "2020-05-13" @default.
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- W3022632962 date "2012-01-01" @default.
- W3022632962 modified "2023-09-26" @default.
- W3022632962 title "Space Propulsion" @default.
- W3022632962 cites W2001533942 @default.
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- W3022632962 doi "https://doi.org/10.1016/b978-1-85617-912-6.00014-1" @default.
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