Vostok (Russian: Восток, lit. 'East') was a family of rockets derived from the Soviet R-7 Semyorka ICBM and was designed for the human spaceflight programme. This family of rockets launched the first artificial satellite (Sputnik 1) and the first crewed spacecraft (Vostok) in human history. It was a subset of the R-7 family of rockets. On March 18, 1980, a Vostok-2M rocket exploded on its launch pad at Plesetsk during a fueling operation, killing 48 people. An investigation into a similar – but avoided – accident revealed that the substitution of lead-based for tin-based solder in hydrogen peroxide filters allowed the breakdown of the H2O2, thus causing the resultant explosion.
Variants The major versions of the rocket were:
Luna 8K72 – used to launch the early Luna spacecraft Vostok-L 8K72 – Variant of the Luna, used to launch prototype Vostok spacecraft Vostok-K 8K72K – a refined version of the above. This was the version actually used for human spaceflight Vostok-2 8A92 – used for launching Zenit reconnaissance satellites throughout the 1960s Vostok-2M 8A92M – modified version for launching Meteor weather satellites into higher orbits. Soyuz/Vostok 11A110 – hybrid of Soyuz and Vostok rockets used as an interim for two launches
Vostok 8K72K Source:
First Stage — Block B, V, G, D (four strap-on boosters) Gross mass: 43,300 kg Empty mass: 3,710 kg Thrust (vac): 4 x 99,000 kgf (971 kN) = 3.88 MN Isp: 313 seconds (3.07 km/s) Burn time: 118 s Isp(sl): 256 seconds (2.51 km/s) Diameter: 2.68 m Span: 8.35 m Length: 19.00 m Propellants: Lox/Kerosene Engines: 1 x RD-107-8D74-1959 per booster = 4 Second Stage — Block A (core stage) Gross mass: 100,400 kg Empty mass: 6,800 kg Thrust (vac): 912 kN Isp: 315 seconds (3.09 km/s) Burn time: 301 s Isp(sl): 248 seconds (2.43 km/s) Diameter: 2.99 m Length: 28.00 m Propellants: Lox/Kerosene Engine: 1 x RD-108-8D75-1959 Third Stage — Block E Gross mass: 7,775 kg Empty mass: 1,440 kg Thrust (vac): 54.5 kN Isp: 326 seconds (3.20 km/s) Burn time: 365 s Diameter: 2.56 m Span: 2.56 m Length: 2.84 m Propellants: Lox/Kerosene Engine: 1 x RD-0109
Gallery
See also
Vostok 1 Vostok programme Vostok spacecraft
Notes
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