The
Svitiaz aerospace rocket complex (ASRC) is intended for injection of various
spacecrafts (SC) into circular, elliptic and high-altitude circular orbits including
the geostationary one (GSO).
The ASRC contains:
- aerospace system (ACS) composed of an aircraft-carrier (AC) and launch vehicle
(LV) installed on the latter.
- technical complex of the LV located on the base airport and intended for LV
preparation to the launch;
- technical complex of the AC intended for AC preparation to the service and
periodical handling;
- ground complex of control and telemetry measurement intended for flight control
and processing of telemetry data received from the flying system.
The aircraft-carrier An-225-100 is elaborated by the Aviation Scientific-Technical
Complex named after O. Antonov. It is modification of the base aircraft An-225
Mriya. The aircraft is equipped by special devices to secure the LV above the
fuselage. In the pressure-tight cabins the onboard equipment and launch operators
are located. The Svitiaz LV is being created on the basis of units, aggregates
and systems from Zenit LV. It consists of three stages on non-toxic propellants
- liquid oxygen and kerosene. To the geostationary orbit the launch vehicle
is injected under use a solid-propellant apogee stage.
· Not high technical risk of elaboration owing to application of proven technologies.
· No need to construct expensive launch facilities..
· Possibility of wide selection of the launch point and orbit inclination.
· Possibility of self-transportation of the system.
· Ecologically clean propellants.
Power characteristics of Svitiaz ACS

| Maximum take-off mass of the system, t |
600
|
| LV maximum lift-off mass, t |
250
|
| LV propellants:oxidizerfuel |
liquid oxygenkerosene RG-1
|
|
Number of stages
Number of stages at launches into GSO
|
|
|
Payload mass injected into an orbit, kg:
ISS orbit: Hcirc=400 km; i=51.6°
transfer to GSO
GSO
|
|
| LV propellant mass, t |
210
|
| Engines thrust during LV start, tf |
355
|
| Runway length, m |
3800
|
| LV full length, m |
40
|
| LV wing span, m |
15
|
| Diameter of LV stages (1st and 2nd), m |
3,9
|
| Diameter of LV nose fairing, m |
3,9
|
Layout scheme

Svitiaz ASC represents a unique system that allows launches of spacecrafts without complicated ground infrastructure of the Space Centers.
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