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Dnepr LV Performance
Dnepr LV Performance Characteristics for Circular Orbits (kg)
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Launch
Base
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Orbit
Altitude, km
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98о Inclination
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65о Inclination
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Standard SHM
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Extended SHM
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Standard SHM
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Extended SHM
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Payload mass, kg
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Yasny
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300
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1800 |
1650 |
3200 |
2950 |
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Baikonur
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1500 |
1450 |
- |
- |
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Yasny
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400 |
2000 |
1850 |
2950 |
2700 |
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Baikonur
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1700 |
1470 |
- |
- |
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Yasny
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500 |
2100 |
1850 |
2650 |
2400 |
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Baikonur
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1650 |
1450 |
- |
- |
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Yasny
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600 |
1700 |
1500 |
2000 |
1800 |
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Baikonur
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1350 |
1150 |
- |
- |
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Yasny
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700 |
1100 |
1000 |
1350 |
1200 |
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Baikonur
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800 |
750 |
- |
- |
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Yasny
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800 |
600 |
450 |
700 |
600 |
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Baikonur
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450 |
350 |
- |
- |
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Контакты
7 Sergey Makeev St., bld.2, Moscow 123100, Russian Federation
Telephone: +7 (495) 745-72-61
Fax: +7 (495) 232-34-85
E-mail: info@kosmotras.ru
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Dnepr Program
During 1992-2003 timeframe, a team of Russian and Ukrainian companies together with the Russian Ministry of Defense (MoD) were involved in developing a commercial space launch system based on the technology of the SS-18 ICBMs being withdrawn from service.
Description and main specifications |
Ракета РС-20
Description and main specifications
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| Создание сайта Web2b
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