Temp-2S, 15Ž42, RS-14, SS-16 Sinner
Basic data
The beginning of the development:
10. July 1969
Design office:
The moscow institute of thermal (thermal) technologies
Manufacturer: Votkinský race
Flight test:
the beginning of the year 1972 - the end 1974 (another source 1972 - 1976)
RT-2P - January 1970 - January 1972
Combat duty:
21. February 1976
Entry into service:
it has not been approved in the service of the
Number of degrees: 3
Propulsion: solid fuel
Launchers:
mobile launchers placed on the vehicle
The number of warheads and power: 1x0.65 - 1.5 Mt
Combat load: 940 kg
Maximum range: 9000 km
Guide: autonomous inertial
Accuracy:
the maximum error of 1.2 - 1.6 km
Length:
18.5 m
Maximum diameter: 1.79 m
Starting weight: 37.0 t
The mass of the fuel:
Oxidant: -
Fuel: -
Thrust (sea level/vacuum):
Specific impulse (sea level/vacuum):
Preparing to launch:
Life:
Source: Russian Strategic Nuclear Forces, Pavel Podvig, Oleg Bukharin, MIT Press, Cambridge, 2001
(original: Raketnije troops strategičeskogo naznačenija).
Basic data
The beginning of the development:
10. July 1969
Design office:
The moscow institute of thermal (thermal) technologies
Manufacturer: Votkinský race
Flight test:
the beginning of the year 1972 - the end 1974 (another source 1972 - 1976)
RT-2P - January 1970 - January 1972
Combat duty:
21. February 1976
Entry into service:
it has not been approved in the service of the
Number of degrees: 3
Propulsion: solid fuel
Launchers:
mobile launchers placed on the vehicle
The number of warheads and power: 1x0.65 - 1.5 Mt
Combat load: 940 kg
Maximum range: 9000 km
Guide: autonomous inertial
Accuracy:
the maximum error of 1.2 - 1.6 km
Length:
18.5 m
Maximum diameter: 1.79 m
Starting weight: 37.0 t
The mass of the fuel:
Oxidant: -
Fuel: -
Thrust (sea level/vacuum):
Specific impulse (sea level/vacuum):
Preparing to launch:
Life:
Source: Russian Strategic Nuclear Forces, Pavel Podvig, Oleg Bukharin, MIT Press, Cambridge, 2001
(original: Raketnije troops strategičeskogo naznačenija).