Lightweight launch vehicle for launching of 200 kg in 800 km
Use of the innovative materials and industrial components make it possible to achieve a relatively low cost of launces. High technological effectiveness of all rocket’s components allows to provide the efficiency of launching services.
Modern and efficient fuel components.
Minimization of dry mass by using the composite materials.
Simplification of development and cost reduction due to additive technologies.
The use of electric pump units.
Reactive landing of the first stage.
Maximum unification of elements and units of the first and second stages.
Technical specifications:
Basic characteristics of the launch vehicle
Launching weight, kg – 17500
Payload weight in the sun-synchronous orbit of 800 km height, kg – 200
Payload weight in the low orbit of 200 km height and inclination of 51,7, kg – 335
Basic characteristics of stage 1
Weight, kg – 15020
Fuel components weight, kg – 12914
Number and type of engines – 9 liquid-propellant rocket engines
On-Earth thrust/vacuum thrust, tf– 21,9/27,0
Running time, sec – 150
On-Earth/vacuum specific impulse, s – 263/324
Basic characteristics of stage 2
Weight, kg – 2832
Fuel components weight, kg – 2480
Number and type of engines – 1 liquid-propellant rocket engine
On-Earth thrust/vacuum thrust, tf – -/3,3
Running time, sec – 221
On-Earth/vacuum specific impulse, s – -/365
Specifications
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