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Sputnik (rocket)

释义

Specifications
Sputnik 8A91
Sputnik specifications
References

{{for|the Sputnik 11A59 rocket|Polyot (rocket)}}{{distinguish|Sputnik 1}}{{Infobox Rocket
|image = Sputnik 8K71PS grey.svg
|imsize = 180
|caption = Sputnik Rocket
|name = Sputnik (8K71PS/8A91)
|function = Early (first) carrier rocket
|manufacturer = OKB-1
|country-origin = USSR
|height = 8K71PS: {{convert|30.0|m|ft|lk=on|abbr=on}}
8A91: {{convert|31.1|m|ft|abbr=on}}
|diameter = {{convert|2.99|m|ft|abbr=on}}
|mass = {{convert|267000|kg|lb|abbr=on}}
8A91: {{convert|269300|kg|lb|abbr=on}}
|stages = 2
|capacities =
|location=LEO (8K71PS)
|kilos = 8K71PS: {{convert|500|kg|lb|abbr=on}}
8A91: {{convert|1327|kg|lb|abbr=on}}
|family = R-7
|comparable = Vanguard
Juno I
|status = Retired
|sites = LC-1/5, Baikonur
|launches = 4 (2 8K71PS, 2 8A91)
|success = 3
|fail = 1 (8A91)
|first = 8K71PS: 4 October 1957
8A91: 27 April 1958
|last = 8K71PS: 3 November 1957
8A91: 15 May 1958
|payloads = Sputnik 1
Sputnik 2
Sputnik 3
|stagedata =
|type = booster
|stageno =
|diff = Block B, V, G, D
|number = 4
|engines = 1 RD-107
|thrust = {{convert|970|kN|lbf|lk=on|abbr=on}}
|SI = 306 s
|burntime = 120 s
|fuel = LOX/Kerosene

  }}  {{Infobox Rocket/Stage

|type = stage
|stageno = First
|diff = Block A
|engines = 1 RD-108
|thrust = {{convert|912|kN|lbf|lk=on|abbr=on}}
|SI = 308 s
|burntime = 330 s
|fuel = LOX/Kerosene

The Sputnik rocket was an unmanned orbital carrier rocket designed by Sergei Korolev in the Soviet Union, derived from the R-7 Semyorka ICBM. On 4 October 1957, it was used to perform the world's first satellite launch, placing Sputnik 1 into a low Earth orbit.

Two versions of the Sputnik were built, the Sputnik-PS (GRAU index 8K71PS), which was used to launch Sputnik 1 and later Sputnik 2, and the Sputnik (8A91), which failed to launch a satellite in April 1958, and subsequently launched 3 on 15 May 1958.^[1]

A later member of the R-7 family, the Polyot, used the same configuration as the Sputnik rocket, but was constructed from Voskhod components. Because of the similarity, the Polyot was sometimes known as the Sputnik 11A59.

Specifications

First Stage: Block B, V, G, D (four strap-on boosters)
- Gross mass: 43.0 tons
- Empty mass: 3.400 tons
- Thrust (vac): 4 × 99,000 kgf = 396 Mgf (3.89 MN)
- Isp: 306 s (3,000 N·s/kg)
- Burn time: 120 s (2 min)
- Isp (sl): 250 s (2,450 N·s/kg)
- Diameter: {{convert|2.68|m|ft}}
- Span: {{convert|2.68|m|ft}}
- Length: {{convert|19.2|m|ft}} (without nozzles)
- Propellants: LOX/Kerosene
- Engines: 1 x RD-107-8D74PS per booster = 4
Second Stage: Block A (core stage)
- Gross mass: 94.0 tons
- Empty mass: 7.495 tons
- Thrust (vac): 99,000 kgf (970 kN)
- Isp: 308 s (3,020 N·s/kg)
- Burn time: 310 s (5 min 10 s)
- Isp(sl): 241 s (2,360 N·s/kg)
- Diameter: {{convert|2.95|m|ft}}
- Span: {{convert|2.95|m|ft}}
- Length: {{convert|28|m|ft}}
- Propellants: LOX/Kerosene
- Engine: 1 x RD-108-8D75PS
Total mass: 267 tons (534,000 lb)
Total span: {{convert|10.303|m|ft}}
LEO payload: 500 kg
Total liftoff thrust: 3.89 MN

Sputnik 8A91

The Sputnik 8A91 had more powerful 8D76 and 8D77 engines installed,^[2] increasing its payload capacity, and allowing it to launch much heavier satellites than Sputnik 1 and Sputnik 2. It was launched two times, in 1958.^[3] The first launch, on 27 April, failed due to vibrations that unexpectedly occurred during the flight along the longitudinal axis of the rocket. On 15 May, it successfully launched Sputnik 3.^[4]^[5]

Sputnik specifications

Stage number: 0 - Strap-on boosters; 4 x Sputnik 8A91-0
- Gross mass: 43.0 tons
- Empty mass: 3.400 tons
- Thrust (vac): 4 × 99,000 kgf = 396 Mgf (3.89 MN)
- Isp: 310 s (3,040 N·s/kg)
- Burn time: 130 s (2 min 10 s)
- Isp(sl): 252 s (2,470 N·s/kg)
- Diameter: {{convert|2.68|m|ft}}
- Span: {{convert|2.68|m|ft}}
- Length: {{convert|19.2|m|ft}} (without nozzles)
- Propellants: Lox/Kerosene
- Engines: 1 x RD-107-8D76 per booster = 4
Stage number: 1 - Core stage; 1 x Sputnik 8A91-1
- Gross mass: 95.0 tons
- Empty mass: 7.100 tons
- Thrust (vac): 82,000 kgf (804 kN)
- Isp: 315 s (3,090 N·s/kg)
- Burn time: 360 s (6 min)
- Isp(sl): 246 s (2,410 N·s/kg)
- Diameter: {{convert|2.95|m|ft}}
- Length:{{convert|28|m|ft}}
- Propellants: LOX/Kerosene
- Engine: 1 x RD-108-8D77
Total mass: 269.3 tons{{Vague|short, as somebody converted one of them? long? metric?|date=March 2008}}
Total span: {{convert|10.303|m|ft}}
LEO payload: 1,327 kg (2,925 lb)
Total liftoff thrust: 385,950 kgf (3.784 MN, 850,870 lbf)

References

1. ^{{ru icon}} Sputnik Rocket
2. ^{{cite web|url=http://www.lpre.de/energomash/RD-107/index.htm |title=РД-107 и РД-108 | RD-107 and RD-108 |publisher=lpre.de|accessdate=2015-12-24}}
3. ^{{cite web|url=http://planet4589.org/space/log/launchlog.txt |title=Jonathan McDowell's launch log |publisher=planet4589.org|accessdate=2015-12-24}}
4. ^{{ru icon}} Soviet Solar Cells on Orbit
5. ^{{cite web|url=http://www.astronautix.com/craft/sputnik3.htm|title=Sputnik 3|publisher=astronautix.com|accessdate=2015-12-24|deadurl=yes|archiveurl=https://web.archive.org/web/20131108103951/http://www.astronautix.com/craft/sputnik3.htm|archivedate=2013-11-08|df=}}

{{Expendable launch systems}}{{Russian launch vehicles}}{{R-7 rockets}}{{Use British English|date=January 2014}}Sputnik

4 : R-7 (rocket family)|Space launch vehicles of the Soviet Union|Sputnik|Vehicles introduced in 1957

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