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Vostok (rocket family)

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Vostok
Vostok 8K72K rocket on display in Moscow at the Exhibition of Achievements of National Economy
FunctionSmall-lift launch vehicle
ManufacturerOKB-1 / RKTs Progress
Country of originSoviet Union
Size
Mass280,000–290,000 kg (620,000–640,000 lb)
Stages3
Capacity
Payload to LEO
Mass4,725 kg (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
Boosters (First stage) – Block B, V, G & D[a]
No. boosters4
Powered by1 × RD-107-8D74-1959
Maximum thrust970.86 kN (218,260 lbf)
Total thrust3,883.44 kN (873,030 lbf)
Specific impulse256 s (2.51 km/s)
Burn time118 seconds
PropellantLOX / Kerosene
Second stage (core) – Block A
Powered by1 × RD-108-8D75-1959
Maximum thrust912 kN (205,000 lbf)
Specific impulse248 s (2.43 km/s)
Burn time301 seconds
PropellantLOX / Kerosene
Third stage – Block E[b]
Powered by1 × RD-0109
Maximum thrust54.5 kN (12,300 lbf)
Specific impulse326 s (3.20 km/s)
Burn time365 seconds
PropellantLOX / Kerosene

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

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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 99,000 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
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See also

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Notes

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  1. ^ This is a transliteration of the second through fifth letters of the Cyrillic alphabet (Б, В, Г, Д). A sense-for-sense translation would correspond to the second through fifth letters of the Latin alphabet, 'Block B, C, D & E'.
  2. ^ This is a transliteration of the sixth letter of the Cyrillic alphabet (E). A sense-for-sense translation would correspond to the sixth letter of the Latin alphabet, 'Block F'.

References

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  1. ^ a b c "Vostok-L 8K72". www.astronautix.com. Retrieved 2023-07-30.
  2. ^ a b "Vostok 8K72K". www.astronautix.com. Retrieved 2023-07-30.
  3. ^ "Vostok 8A92". www.astronautix.com. Retrieved 2023-07-30.
  4. ^ "Vostok 8A92M". www.astronautix.com. Retrieved 2023-07-30.
  5. ^ "Soyuz 11A510". www.astronautix.com. Retrieved 2023-07-30.