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- W2150213954 abstract "A computer code which rapidly calculates time optimal combined high- and low-thrust transfers between two geocentric orbits in the presence of a strong gravitational field has been developed as a mission analysis tool. The low-thrust portion of the transfer can be between any two arbitrary ellipses. There is an option for including the effect of two initial high-thrust impulses which would raise the spacecraft from a low, initially circular orbit to the initial orbit for the low-thrust portion of the transfer. In addition, the effect of a single final impulse after the low-thrust portion of the transfer may be included. The total Delta V for the initial two impulses must be specified as well as the Delta V for the final impulse. Either solar electric or nuclear electric propulsion can be assumed for the low-thrust phase of the transfer." @default.
- W2150213954 created "2016-06-24" @default.
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- W2150213954 date "1974-08-05" @default.
- W2150213954 modified "2023-09-23" @default.
- W2150213954 title "Optimal high- and low-thrust geocentric transfer" @default.
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- W2150213954 doi "https://doi.org/10.2514/6.1974-801" @default.
- W2150213954 hasPublicationYear "1974" @default.
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