
R-5
R-5M
DF-2
DF-2A |
Rocket R-5M became the first domestic strategic rocket
carrying a nuclear charge that gave start to the development of the Soviet nuclear-rocket
protection shield.
The R-5M rocket is the successful successor of the German long-range rocket A-4.
The rocket was used also as sounding rockets "W5-A", "W5-W" and "Vertikal".
The R-5 missile started at Korolev's OKB-1. Active phase of the R-5 development
fell on 1952. A single-stage missile was designed as a 20-meter tall cylinder
instead of cigar-like shape common for previous A-4-derived vehicles. For the
first time, both fuel and oxidizer tanks welded of light aluminum and magnesium
alloys were made as monocoque structures yielding great weight savings. The riveting
was used for the assembly of the tail section made of dural and aluminum.
The tail section also carried short triangular fins with wind rudders instead
of bulky A-4-derived stabilizers of the R-1 and 2. Still, resemblance to the
A-4 has been retained in the propulsion unit.
The R-5M was powered by a single A-4-derived engine, developed in OKB-456 in
Khimki under designation RD-103M. It used a 92-percent mix of alcohol with water
as a fuel and liquid oxygen as an oxidizer and yielded trust of 43.85 tons. Comparing
with the A-4 engine, RD-103M featured a number of improvements including better
cooling system for the combustion chamber and introduction of automated trust
control. Solid catalizator was used for decay of hydrogen peroxide in the gas
generator, which provided hot gas to drive the turbopump on the propellant line.
The centrifugal pump was used to drive the hydrogen peroxide into the gas generator.
Elastic fuel lines were also used for the first time.
The R-5M flight control system included aerodynamic and gas rudders, which prevented
the rocket from rolling about its main axis. After the engine cutoff, the stabilization
would be still maintained using the oxygen gas which during the active flight
served for pressurization of the oxidizer tank. To achieve this, the pressurization
gas was directed into the system of nozzles placed in the conical section, connecting
the warhead with the rest of the rocket body.
Weighing 28,570 kg at launch, the R-5M was able to reach a 1,200-km distance
becoming first "strategic" missile in the Soviet arsenal.
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The R-5M was exported as
weapon to China and was here named DF-2 and DF-2A.
Development of a nuclear warhead that could be
delivered by the missile began in 1964. In late 1966, a series of flight tests
using the DF-2 missile integrated with a dummy warhead were carried out to test
the reliability of the warhead design. On 27 October 1966, a specially modified
Dongfeng 2A missile carrying a nuclear warhead successfully detonated in the
Lop Nor nuclear test site.
| |
R-5 |
R-5M |
DF-2 |
DF-2A |
| Length total |
22.12 m |
20.75 m |
21.31 m |
~23.50 m |
| Length without control unit/ warhead |
17.37 m |
17.37 m |
17.37 m |
~18.5 m |
| Diameter |
1.65 m |
1.65 m |
1.65 m |
1.65 m |
| Propellant |
--------------------92%
Ethyl-Alcohol / LOX ------------------
|
| Mass propellant (t) |
24.34 |
24.73 |
24.73 |
26.72 |
| Engine |
RD-103
|
RD-103M
|
RD-103M
|
RD-103M
|
| Thrust s.l. (kN) |
415.7 |
430.1 |
430.1 |
430.1 |
| Thrust vac (kN) |
469.7 |
484.9 |
484.9 |
484.9 |
| Isp s.l. (Ns/kg) |
2118 |
2158 |
2158 |
2158 |
| Isp vac Ns/kg) |
2393 |
2432 |
2432 |
2432 |
| Burn time, nominal (sec) |
124 |
124 |
124 |
134 |
| Total vacuum impulse (MNs) |
58.2 |
60.2 |
60.2 |
65.0 |
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