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SOYUZ-2-1V Launch Vehicle
"Soyuz-2-1 V " launch vehicle is two-stage light class launch vehicle developed for spacecraft launches from launching facilities which are meant for “Soyuz-2” launch vehicle. The launch vehicle is developed on the basis of “Soyuz-2-1V” launch vehicle by removing of strap-on boosters and installing of NK-33A engine on the core module and control engine RD0110R (development of OAO ‘KBHA’). The second stage unit is adopted with updating of “Soyuz-2-1V ” third stage unit.
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SOYUZ-2-1V Launch Vehicle
"Soyuz-2-1 V " launch vehicle is two-stage light class launch vehicle developed for spacecraft launches from launching facilities which are meant for “Soyuz-2” launch vehicle. The launch vehicle is developed on the basis of “Soyuz-2-1V” launch vehicle by removing of strap-on boosters and installing of NK-33A engine on the core module and control engine RD0110R (development of OAO ‘KBHA’). The second stage unit is adopted with updating of “Soyuz-2-1V ” third stage unit.
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SOYUZ-2-1V Launch Vehicle
"Soyuz-2-1 V " launch vehicle is two-stage light class launch vehicle developed for spacecraft launches from launching facilities which are meant for “Soyuz-2” launch vehicle. The launch vehicle is developed on the basis of “Soyuz-2-1V” launch vehicle by removing of strap-on boosters and installing of NK-33A engine on the core module and control engine RD0110R (development of OAO ‘KBHA’). The second stage unit is adopted with updating of “Soyuz-2-1V ” third stage unit.
SOYUZ-2-1V Launch Vehicle
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"Soyuz-2-1 V " launch vehicle is two-stage light class launch vehicle developed for spacecraft launches from launching facilities which are meant for “Soyuz-2” launch vehicle. The launch vehicle is developed on the basis of “Soyuz-2-1V” launch vehicle by removing of strap-on boosters and installing of NK-33A engine on the core module and control engine RD0110R (development of OAO ‘KBHA’). The second stage unit is adopted with updating of “Soyuz-2-1V ” third stage unit. Light class launch vehicle development associates with growing needs of small spacecraft launches. Creation of "Soyuz-2-1V" launch vehicle using units of “Soyuz-2-1B” as well as existing technical and launching facilities allows dramatic reduction in development, operation and launch associated costs. "Soyuz-2-1V" control system with improved soft- and hardware is used to provide stability, controllability and operation of “Soyuz-2-1V” regulating systems. To interface "Soyuz-2-1V" with launching mechanism the following modifications are made: 4 supports are installed on the first stage unit for supporting booms of launching facility; 4 supports are installed on the first stage’s aft module for guiding system of launching facility. |
SOYUZ-2-1V Launch Vehicle
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Number of stages |
2 |
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Maximal length |
44 m |
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Maximal unit diameter |
2,95 m |
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Nose Fairing diameter |
3 m |
SOYUZ-2-1V Launch Vehicle
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Lifting capacity of "Soyuz-2-1V" launch vehicle at the time of its injection into low orbit ( Нcyr=200) (LEO)
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