LAUNCH VEHICLE OF COMBINED CONFIGURATION

LAUNCH VEHICLE OF COMBINED CONFIGURATION

rocketry and space engineering; injection of payloads into near-earth orbit. SUBSTANCE: launch vehicle includes lower polypod stack consisting of central and side rocket pods, compartment for securing higher stage of rocket and attachment system for securing the side pods with central pod and second...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MEDVEDEV A.A, DERMICHEV G.D, KISELEV A.I, KARRASK V.K, FILIPPOV S.N, PETROKOVSKIJ S.A
Format: Patent
Sprache:eng
Schlagworte:
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:rocketry and space engineering; injection of payloads into near-earth orbit. SUBSTANCE: launch vehicle includes lower polypod stack consisting of central and side rocket pods, compartment for securing higher stage of rocket and attachment system for securing the side pods with central pod and second belt of attachment units which connect lower parts of side rocket pods with central pod. Provision is made for system of quick separation and withdrawal of side pods from central one. Side rocket pods are identical to central one; attachment system is provided with third belt of attachment units taking up transversal loads, thus forming three-support system for attachment of side pods to central one. Attachment units of third belt are located on upper load-bearing rings of side and central rocket pods. EFFECT: reduced expenses for injection of payloads into orbits due to enhanced power and mass characteristics, unification and simplification of system. 9 cl, 12 dwg