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Dnepr LV Performance

Dnepr LV Performance Characteristics for Circular Orbits (kg)

 

Launch

Base

Orbit

Altitude, km

98о Inclination

65о Inclination

Standard SHM

Extended SHM

Standard SHM

Extended SHM

 Payload mass, kg

 Yasny

300
1800 1650 3200 2950

 Baikonur 

1500 1450 - -

 Yasny

400 2000 1850 2950 2700

 Baikonur   

1700 1470 - -

 Yasny

500 2100 1850 2650 2400

 Baikonur   

1650 1450 - -

 Yasny

600 1700 1500 2000 1800

 Baikonur   

1350 1150 - -

 Yasny  

700 1100 1000 1350 1200

 Baikonur   

800 750 - -

 Yasny  

800 600 450 700 600

 Baikonur   

450 350 - -

 

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

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(MoD) were involved in developing a commercial space launch system based on the technology of the SS-18 ICBMs being withdrawn from service.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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