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Vostok (rocket family)

From Wikipedia, the free encyclopedia
Series of six manned and unmanned Soviet orbiting spacecraft
Vostok
Vostok 8K72K rocket on display in Moscow at theExhibition of Achievements of National Economy
FunctionCarrier rocket
ManufacturerRKK Energia
Country of originSoviet Union
Size
Mass280,000–290,000 kg (620,000–640,000 lb)
Stages3
Capacity
Payload toLEO
Mass4,725 kilograms (10,417 lb)
Associated rockets
FamilyR-7
ComparableAtlas
Titan
Launch history
StatusRetired
Launch sitesBaikonur:LC-1/5,31/6
Plesetsk:LC-41/1,43/3, 43/4
Total launchesVostok-L: 4
Vostok-K: 13
Vostok-2: 45
Vostok-2M: 94
Soyuz/Vostok: 2
Success(es)Vostok-L: 3
Vostok-K: 11
Vostok-2: 40
Vostok-2M: 92
Soyuz/Vostok: 2
Failure(s)Vostok-L: 1
Vostok-K: 2
Vostok-2: 5
Vostok-2M: 2
First flight15 May 1960 (Vostok-L)
Last flight29 August 1991 (Vostok-2M)
Carries passengers or cargoVostok
Zenit
Meteor
First stage (Block B, V, G, D)
Powered by1RD-107-8D74-1959
Maximum thrust970.86 kN
Burn time118 seconds
PropellantKerosene/LOX
Second stage (Block A)
Powered by1RD-108-8D75-1959
Maximum thrust912 kN
Burn time301 seconds
PropellantRP-1/LOX
Third stage (Block E)
Powered by1RD-0109
Maximum thrust54.5 kN
Burn time365 seconds
PropellantKerosene/LOX

Vostok (Russian: Восток, translated as "East") was a family of rockets derived from theSovietR-7 SemyorkaICBM and was designed for thehuman spaceflightprogramme. 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 theR-7 family of rockets.

On March 18, 1980, a Vostok-2M rocketexploded on its launch pad atPlesetsk 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 inhydrogen peroxide filters allowed the breakdown of the H2O2, thus causing the resultant explosion.

Variants

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The major versions of the rocket were:

Vostok 8K72K[2][1]

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  • 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 99,000kgf (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 xRD-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

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See also

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References

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  1. ^abc"Vostok-L 8K72".www.astronautix.com. Retrieved2023-07-30.
  2. ^ab"Vostok 8K72K".www.astronautix.com. Retrieved2023-07-30.
  3. ^"Vostok 8A92".www.astronautix.com. Retrieved2023-07-30.
  4. ^"Vostok 8A92M".www.astronautix.com. Retrieved2023-07-30.
  5. ^"Soyuz 11A510".www.astronautix.com. Retrieved2023-07-30.
Active
In development
Retired
Cancelled (no launch attempts)
Current
In development
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Classes
  • This template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
  • Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
Missiles
Launch systems
Vostok
Molniya
Soyuz
Soyuz 2
Launch sites
Launches
Engines
See also


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