VERFAHREN UM EINE NUTZLAST IN ORBIT ZU BRINGEN MITTELS EINER HYBRIDEN MULTIFUNKTIONELLEN MIT EINEM FLÜSSIGBRENNSTOFFRAKETENANTRIEBSSYSTEM AUSGERÜSTETEN TRÄGERRAKETE

The invention relates to the field of rocket-space engineering and may find application during the development of rocket-space systems serving to place manned and unmanned space ships into a near-earth orbit. The launch vehicle of a combined scheme comprises a lower multiunit assembly of RUs, compos...

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Bibliographische Detailangaben
Hauptverfasser:	MEDVEDEV, ALEXANDR ALEXEEVICH, PETROKOVSKY, SERGEI ALEXANDROVICH, MOTORNY, EVGENY IVANOVICH, DERMICHEV, GENNADY DMITRIEVICH, RADUGIN, IGOR SERGEEVICH, KARRASK, VLADIMIR KONSTANTINOVICH, JURIEV, VASILY JURIEVICH, KISELEV, ANATOLY IVANOVICH
Format:	Patent
Sprache:	ger
Schlagworte:	AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to the field of rocket-space engineering and may find application during the development of rocket-space systems serving to place manned and unmanned space ships into a near-earth orbit. The launch vehicle of a combined scheme comprises a lower multiunit assembly of RUs, composed of identical RUs, wherein the side RUs are mounted on the central RU symmetrically relative to its longitudinal axis in sectors formed by the swinging planes of the LRES of the central RU.