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Shtil (R-29RM) |
Makeev State Rocket Center * Babakin Science and Research Center
The Shtil is an ballistic
missile, designated the R-29RM or RSM-54. It is a two-stage liquid fueled missile,
capable of deploying small spacecraft in LEO. The Shtil-1 uses the warhead fairing
to hold the spacecraft, whereas the Shtil-2 (length 18, 4 m) has a larger separating
fairing to hold larger spacecraft. Shtil-2 can be launched from ground-based launch
table. The Makeyev Design Bureau
has proposed an air-launched version Shtil-3A (lift-off mass 45,6 tons, length
18,7 m, payload for LEO 0,95 ton).
All two stages are liquid-fuelled with storable UDMH/N2O4 propellants. The engines
are nestled inside the propellant tanks, rather than below them to save space. Upper
and lower bulkheads have unusual shapes to accommodate engines with minimal interstage
space.
A number of launch vehicles are being developed now on the basis of technologies
and components of RSM-54 missile. These launch vehicles
can be launched from the launch tubes of submarines or from the ground-based launch
complex located at the northern part of Arkhangelsk region.
The family of Shtil light-class LV includes the following
launch vehicles: SHTIL -1, SHTIL-2.1, SHTIL-2 and
SHTIL-3.
The space rocket system includes:
In July 1998
the Shtil LV has injected two German
Tubsat satellites into the near-earth orbit.
The launch was made from the Barents Sea by
a not dived submarine.
In
Shtil-2.1 launch
vehicle the payload is placed in a special section mounted on the front frame of
instrument section. The special section is an assembly consisting of fairing presented
by the standard astro-dome of the RSM-54 missile and
a coupling section. The coupling section provides for the joining of the payload
section and the missile and for the accommodation of the spacecraft.
In Shtil-2R
launch vehicle the payload is placed in a special section, which is installed in
the LV nose part and comprises nose fairing and adapter used to join the section
to the launch vehicle. The newly developed nose fairing protects the payload from
dust and moisture and is equipped with a separation and jettison system. The cover
of the fairing has hatches to connect the payload with the equipment of ground-based
launch complex. For the purpose to increase the Launch Vehicle capacity a small-size
upper-stage engine is placed in payload section.
The
Shtil-3
launch vehicle is the most powerful missile in the Shtil
family. In this case the combat missile was retrofitted as follows:
new design of the third stage with more fuel stock was developed;
new instrument section was developed;
additional injection stage was installed. It passed through a whole cycle of testing;
new payload section was developed ;
new on-board measuring complex was developed.
Launch vehicles |
Shtil -1 |
Shtil-2.1 |
Shtil-2R |
Shtil-3 |
Number of stages |
3 |
3 |
3 |
3 + booster |
Missile dimensions, m: |
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|
|
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Launching weight, t |
39.3 |
39.7 |
40 |
44 |
Volume of payload (capsule) zone, m3 |
0.195 |
0.25 |
1.17 |
3.6 |
Characteristics for the case
of injections into circular orbits with inclination of 79 deg.: |
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|
|
|
Method of launch |
ground-based launching complex, submarine |
ground-based launching complex |
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Propellant |
liquid, long-storage |
Shtil-K
A new LV Shtil-K can be launched from ground-based
launch table. The upper stage Kaplya is intended for Shtil-K launch vehicle. LV
Shtil-K is being developed on the base of RSM-54 missile. It is designed to
launch spacecraft into the near-Earth orbit. First two stages developed at the State
Rocket Center "Makeyev Design Bureau" and upper composite, which is being under
development at Babakin Science and Research Space Center. Upper composite includes
the upper stage Kaplya, payload adapter and fairing. Upper stage Kaplya is being
developed on the base of elements of the Fregat upper stage.