### 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 |

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### ASJC Scopus subject areas

- Engineering(all)

### Cite this

*Cosmic Res*(4 ed., Vol. 13, pp. 425-431)

**OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS.** / Shklyar, V. N.; Malyshenko, A. M.

Research output: Chapter in Book/Report/Conference proceeding › Chapter

*Cosmic Res.*4 edn, vol. 13, pp. 425-431.

}

TY - CHAP

T1 - OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS.

AU - Shklyar, V. N.

AU - Malyshenko, A. M.

PY - 1975/7

Y1 - 1975/7

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=0016525721&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0016525721&partnerID=8YFLogxK

M3 - Chapter

VL - 13

SP - 425

EP - 431

BT - Cosmic Res

ER -