Sever (spacecraft)

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Soyuz Sever (Siber)
One of the conceptual drawings of Sever space station (OS-1962) and Sever ferry (early Soyuz) from 1962
ManufacturerExperimental Design Bureau
(OKB-1)
Country of originSoviet Union
OperatorSoviet space program
ApplicationsCrewed spacecraft
Specifications
PowerSolar arrays
RegimeLow Earth orbit
(with boosters lunar)
Production
StatusDesign proposals
Built0
Launched0
Related spacecraft
Derivatives

Soyuz 7K-OK
Soyuz-A

Soyuz-B

Soyuz Sever, also spelled Soyuz Siber, (translates to Soyuz north), was an early (1959–1962) design of the Soyuz spacecraft. The Soyuz Sever design of a crewed spacecraft started the Soyuz programme. In 1956, the Soyuz Sever spacecraft was proposed as the replacement for the Vostok spacecraft. Vostok spacecraft had only a crew of one; the Soyuz Sever plan would have crew of three. Sever was planned to be launched on a R7 rocket or Vostok rocket. The Sever plans were made by the Experimental Design Bureau (OKB-1) of the Soviet Union. While the Sever spacecraft was never built and launched, many of the designs and testing outcomes became part of the first generation Soyuz spacecraft, Soyuz 7K-OK and the Soyuz 1 mission launched on 23 April 1967. Sever (Sever ferry) final plan was to take crews to a Sever space station, OS-1962.[1][2][3]

Design

On 1 March 1959 the first proposal of OKB-1's engineer, Konstantin Feoktistov was for Sever to be twice as large as the final Soyuz spacecraft.[4] The larger size was so Sever could be part of the Soviet future lunar program, the L4-1960 crewed lunar orbiter proposal. This was change so Sever would become a small (Soyuz size) three crewed spacecraft, by August 1959. In 1961, OKB-1 has several new designs for a three-man spacecraft: Sever, and competing esigns: Sever L1-1960 became crewed obiter Soyuz-A, Soyuz-B (orbital tug), Soyuz-V, and Vostok-Zh/Vostok-7. The one of Sever designs would use a lifting body for lift off Earth to reduce crew G forces, as The Spaceship Company does and land more like the Space Shuttle. In 1961, Sever was still a part of the future lunar program. Other plans for Soyuz Sever was a crewed orbital space tug version, so spacecraft could be assembled in low earth orbit. This could be used as step to the moon. The assembled craft would have five rocket boosters assembled together to give enough power to go the moon. This plan was not taken up. The plan did develop Sever into two versions: one with one solar array and one with two solar arrays, the version that is in Soyuz. In 1961 Konstantin Vershinin, commander-in-chief of the Soviet Air Force, setup new requirements for the next generation spacecraft: crew of 2 cosmonauts, launch mass of 5896 to 6350 kg, able to manoeuvre at altitudes of 270 km to 300 km, restartable engines, 15 to 20 days duration, redundant communication radios, in a pressurized re-entry space capsule.[5] Soviet engineer, Vladimir Chelomey, was still pushing for the lifting body spaceplane, but his plan was rejected. On 10 February 1962 a mockup-prototype of the Sever spacecraft with two crew members was completed and a 15-day test was started. The test was planned and led by chief spacecraft designer, Grigoriy Ivanovich Voronin at GKNII in Akhtubinsk. The 1962 proposal included L1-1962, a crewed lunar flyby spacecraft. The some of the 1962 L1-1962 proposal became part of the Soyuz spacecraft.[1][6][2][3]

Designated Sever proposals

Some of the Sever proposals were formalized and given designated projects numbers:

  • L1-1960 Sever crewed circumlunar spacecraft proposal from 1960. This became the Soyuz-A design. L1-1960 was proposed by Sergei Korolev in January 1960. The L1-1960 was a planned three crewed 5,000 to 6,000 kg spacecraft that loop around the moon and then back to earth in 1964, as Apollo 8 did in 1968. L1-1960 would use the N1 rocket that started planning in May 1961.[7][8]
  • L4-1960 Sever crewed lunar orbiter proposal from 1960 with a gross mass of 12,000 kg, proposed by Korolev in January 1960. The L4-1960 lunar orbiter would be two times the size of L1-1960. L4-1960 would also use the N1 rocket. The L4-1960 would have payload of 6,000 to 8,000 kg.[9]
  • L1-1962 Sever crewed lunar flyby spacecraft proposal from 1962, some of design used in finial Soyuz. L1-1962 was planned lunar flyby spacecraft from 1962. In L1-1962 a Vostok-Zh crews, cosmonaut assemblymen, space tug would assemble three rocket stages, rocket blocks (RB), in orbit. On top of the rocket stages would be the Soyuz Sever L1 to travel to the moon. Status: Study 1962. The L1-1962 had a gross mass of 16,500 kg. Vostok-Zh was also planned to be the craft to assemble the Sever spacestation, OS-1962. With Sever to be the ferry craft to take crews to and from the spacesttion.[10]

OS-1962 space station

Part of the Soviet space station Sever project was the planning of a crewed space station, the OS-1962 design plan (Orbital Station 1962). Korolev approved the OS-1962 project called the "Complex docking of spacecraft in earth orbit - Soyuz" on 10 March 1962. The plan also included the L1-1960, circumlunar spacecraft proposal project. The OS-1962 space station plan called for station with a gross mass of 13,500 kg. The OS-1962 plan first had the large spacecraft, which was later reduced by half. The space station was to be placed in orbit with three R-7 rocket launches and Vostok-7 spacecraft. OS-1962 was to be a platform for earth observation. The OS-1962 space station would have ZhO living section, the BAA scientific apparatus block, and the Sever (Soyuz) spacecraft docked to the space station. The OS-1962 station had four solar arrays for power. While OS-1962 was not built some of its designs were used in later space stations.[11][12] The OP space station (1962),[13] OS-1 space station (1965),[14][15] Soyuz R space station (1966)[16] and MKBS space station (1974) also were not built.[17][18] Salyut 1 became the Soviet Union's first space station in 1971.[19]

  • L1-1960 Sever was developed into the Soyuz-A and Soyuz-B design the Soyuz 7K-9K-11K circumlunar concept. The drawing shows Soyuz 7K (right), Soyuz 9K booster, and Soyuz 11K tanker with twin whip antennas (left).
    L1-1960 Sever was developed into the Soyuz-A and Soyuz-B design the Soyuz 7K-9K-11K circumlunar concept. The drawing shows Soyuz 7K (right), Soyuz 9K booster, and Soyuz 11K tanker with twin whip antennas (left).
  • Soyuz 7K-OK(A), first working Soyuz, that used many Sever designs. First Soyuz 7K-OK was launched on 23 April 1967.
    Soyuz 7K-OK(A), first working Soyuz, that used many Sever designs. First Soyuz 7K-OK was launched on 23 April 1967.
  • Soyuz family tree, Sever would be at the very top above A / 7K, as A / 7K came from the Sever project
    Soyuz family tree, Sever would be at the very top above A / 7K, as A / 7K came from the Sever project

See also

References

  1. ^ a b "Sever". www.astronautix.com.
  2. ^ a b "NASA, Soyuz History, nasa.gov" (PDF).
  3. ^ a b I. B. Afanasyev, “Unknown Spacecraft (From the History of the Soviet Space Program),” What's New In Life, Science, and Technology: Space Program and Astronomy Series, No. 12, December 1991. Translated in JPRS Report, Science & Technology, Central Eurasia: Space (JPRS-USP-92003), May 27, 1992, p.6
  4. ^ "Feoktistov". www.astronautix.com.
  5. ^ "Vershinin". www.astronautix.com.
  6. ^ "Voronin". www.astronautix.com.
  7. ^ "L1-1960". www.astronautix.com.
  8. ^ Pike, John. "L-1 Lunar Circumnavigation Mission". GlobalSecurity.org. Retrieved 30 June 2009.
  9. ^ "L4-1960". www.astronautix.com.
  10. ^ "L1-1962". www.astronautix.com.
  11. ^ "OS-1962". www.astronautix.com.
  12. ^ "Vostok-Zh". www.astronautix.com.
  13. ^ "OP". www.astronautix.com.
  14. ^ "OS-1 (1965)". www.astronautix.com.
  15. ^ "OS-1 (1969)". www.astronautix.com.
  16. ^ "Soyuz R". www.astronautix.com.
  17. ^ "MKBS". www.astronautix.com.
  18. ^ "MKBS - Secret Origin of Mir and Soyuz T". www.astronautix.com.
  19. ^ Chladek, Jay (2017). Outposts on the Frontier: A Fifty-Year History of Space Stations. University of Nebraska Press. pp. 85–86. ISBN 978-0-8032-2292-2.
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