Abstract
The spatial-turning problem for a space vehicle in the class of motions with two time-optimal successive turns is considered. Formulas are obtained to determine the parameters of successive turns and to estimate the rate of response and flow rate of the propulsive mass.
Original language | English |
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Title of host publication | Cosmic Res |
Pages | 425-431 |
Number of pages | 7 |
Volume | 13 |
Edition | 4 |
Publication status | Published - Jul 1975 |
ASJC Scopus subject areas
- Engineering(all)