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Vostok (rocket family)

Series of six manned and unmanned Soviet orbiting spacecraft


Series of six manned and unmanned Soviet orbiting spacecraft

FieldValue
imageSemyorka Rocket R7 by Sergei Korolyov in VDNH Ostankino RAF0540.jpg
captionVostok 8K72K rocket on display in Moscow at the Exhibition of Achievements of National Economy
nameVostok
functionSmall-lift launch vehicle
manufacturerOKB-1 / RKTs Progress
country-originSoviet Union
stages3
capacities{{Infobox Rocket/Payload
locationLEO
kilos4725 kg
mass280,000-290,000 kg
familyR-7
comparableAtlas
Titan
statusRetired
sitesBaikonur: LC-1/5, 31/6
Plesetsk: LC-41/1, 43/3, 43/4
launchesVostok-L: 4
Vostok-K: 13
Vostok-2: 45
Vostok-2M: 94
Soyuz/Vostok: 2
successVostok-L: 3
Vostok-K: 11
Vostok-2: 40
Vostok-2M: 92
Soyuz/Vostok: 2
failVostok-L: 1
Vostok-K: 2
Vostok-2: 5
Vostok-2M: 2
first15 May 1960 (Vostok-L)
last29 August 1991 (Vostok-2M)
payloadsVostok
Zenit
Meteor
typebooster
diffFirst stage
nameBlock B, V, G & D
number4
engines1×RD-107-8D74-1959
thrust970.86 kN
total{{#expr:970.86*4}} kN
SI256 isp
burntime118 seconds
fuelLOX/Kerosene
stagenoSecond
typestage
diffcore
nameBlock A
engines1×RD-108-8D75-1959
thrust912 kN
SI248 isp
burntime301 seconds
fuelLOX/Kerosene
stagenoThird
typestage
nameBlock E
engines1×RD-0109
thrust54.5 kN
SI326 isp
burntime365 seconds
fuelLOX/Kerosene

|country-origin = Soviet Union Titan Plesetsk: LC-41/1, 43/3, 43/4 Vostok-K: 13 Vostok-2: 45 Vostok-2M: 94 Soyuz/Vostok: 2 Vostok-K: 11 Vostok-2: 40 Vostok-2M: 92 Soyuz/Vostok: 2 Vostok-K: 2 Vostok-2: 5 Vostok-2M: 2 Zenit Meteor Vostok () 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 similarbut avoidedaccident 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 isp
    • Burn time: 118 s
    • Isp(sl): 256 isp
    • 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 isp
    • Burn time: 301 s
    • Isp(sl): 248 isp
    • 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 isp
    • Burn time: 365 s
    • Diameter: 2.56 m
    • Span: 2.56 m
    • Length: 2.84 m
    • Propellants: Lox/Kerosene
    • Engine: 1 x RD-0109

Notes

References

References

  1. "Vostok-L 8K72".
  2. "Vostok 8K72K".
  3. "Vostok 8A92".
  4. "Vostok 8A92M".
  5. "Soyuz 11A510".
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