Rutherford's extended formula and optimization of the gravity assists beam modeling in the Solar system | Zendy

Yury Filippovich Golubev | Zendy; А. В. Грушевский | Zendy; В.В. Корянов | Zendy; А. Г. Тучин | Zendy; Д. А. Тучин | Zendy

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Rutherford's extended formula and optimization of the gravity assists beam modeling in the Solar system

Author(s) -

Yury Filippovich Golubev,

А. В. Грушевский,

В.В. Корянов,

А. Г. Тучин,

Д. А. Тучин

Publication year - 2021

Publication title -

keldysh institute preprints

Language(s) - English

Resource type - Journals

eISSN - 2071-2901

pISSN - 2071-2898

DOI - 10.20948/prepr-2021-6

Subject(s) - spacecraft , physics , aerospace engineering , interplanetary spaceflight , solar system , gravitation , planet , beam (structure) , classical mechanics , mechanics , plasma , astrobiology , astronomy , optics , engineering , solar wind , quantum mechanics

The extended Rutherford formula for the gravitational scattering is obtained. Semi-analytical guaranteeing estimates are presented for a sufficient number of a spacecraft’ virtual trajectories in a beam when simulating gravity assist maneuvers around the Solar system massive bodies which are forming the unceasing procedure for searching for the interplanetary ballistic scenarios. A special importance here is assured by the guaranteed synthesis of the bang-bang gravity assist maneuvers chains if it is necessary to change the asymptotic velocity of the spacecraft relative to the planet.

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