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Application

94022030/28, 1994-06-16

(22)

Actual filing date

1994-06-16

(45)

Published

1999-04-10

(72)

Inventor

Besedin V.P.Meshkov V.V.Fetisov V.A.

(73)

Holder

Gosudarstvennyj Raketnyj Tsentr Im.Akademika V.P.Makeeva"

METHOD OF OPERATION OF RECOVERABLE SPACECRAFT Russian patent published in 1999 - IPC

Abstract RU 2128610 C1

FIELD: space engineering; re-entry spacecraft launched as small payloads (up to 1 t) by means of light launch vehicles. SUBSTANCE: before launch, season and time interval at minimum effect of thermodynamic parameters of atmosphere on touch-down dispersion of spacecraft is predicted by ballistic relationships. Depending on scientific and engineering problems to be solved, active life of spacecraft in space is preset. Spacecraft is injected into orbit by time so that the end of active life coincides with above-mentioned season and time interval. EFFECT: enhanced efficiency of search of landed spacecraft and its delivery to base. 1 dwg

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RU 2 128 610 C1

Authors

Besedin V.P.

Meshkov V.V.

Fetisov V.A.

Dates

1999-04-10—Published

1994-06-16—Filed

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