The Cyclone-1M is a lightweight liquid-propellant launch vehicle designed to deliver payloads into low Earth orbits, including sun-synchronous orbits.
The Cyclone-1M will be launched both from a space launch center located in Ukraine and from foreign space launch centers.
Cyclone-1M lightweight launch vehicle. The Cyclone-1M is also developed based on an RD870 engine, but it uses considerable innovation requiring additional development. In particular, a major part of the launch vehicle bearing structure will be made of carbon-based polymer composites, new engines will be developed for the second and third stages, weight of the onboard avionics will be reduced, and commercial off-the-shelf components will be used.
|
Number of stages |
3 |
|
Dimensions, mm |
|
|
Length |
30000 |
|
Stage 1 |
19000 |
|
Stage 2 |
4500 |
|
Stage 3 |
630 |
|
Payload fairing diameter, mm |
2600 |
|
Launch mass (w/o payload), tons |
|
|
Stage 1 |
64.2 |
|
Stage 2 |
7.2 |
|
Stage 3 |
0.3 |
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Propellants |
|
|
Oxidizer |
|
|
Stage 1 |
liquid oxygen |
|
Stage 2 |
liquid oxygen |
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Stage 3 |
- |
|
Fuel |
|
|
Stage 1 |
kerosene |
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Stage 2 |
kerosene |
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Stage 3 |
hydroxylammonium nitrate (HAN) |
|
Thrust: sea level/vacuum, ton-force |
|
|
Stage 1 |
79.7/89.1 |
|
Stage 2 |
4.84 |
|
Stage 3 |
0.02 |
CYCLONE-4 PAYLOAD CAPABILITY INTO CIRCULAR ORBITS
PAYLOAD ACCOMMODATION AREA
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