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

V. N. Shklyar, A. M. Malyshenko

Research output: Chapter in Book/Report/Conference proceedingChapter

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 languageEnglish
Title of host publicationCosmic Res
Pages425-431
Number of pages7
Volume13
Edition4
Publication statusPublished - Jul 1975

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Flow rate

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Shklyar, V. N., & Malyshenko, A. M. (1975). OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS. In 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.

Cosmic Res. Vol. 13 4. ed. 1975. p. 425-431.

Research output: Chapter in Book/Report/Conference proceedingChapter

Shklyar, VN & Malyshenko, AM 1975, OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS. in Cosmic Res. 4 edn, vol. 13, pp. 425-431.
Shklyar VN, Malyshenko AM. OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS. In Cosmic Res. 4 ed. Vol. 13. 1975. p. 425-431
Shklyar, V. N. ; Malyshenko, A. M. / OPTIMAL SPATIAL TURNING OF A SPACE VEHICLE RELATIVE TO CENTER OF MASS. Cosmic Res. Vol. 13 4. ed. 1975. pp. 425-431
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