Comparison of manned space vehicles

A number of different spacecraft have been used to carry people to and from space.

Legend for below table:   [under development] — [retired,canceled] — [operational,inactive]

Spacecraft Origin Manufacturer Range Launch
system
Crew
size
Length (m) Diameter (m) Launch mass (kg) Power
system
Generated
power (W)
First
flight
Last
flight
Flights*
Apollo  USA North American Aviation
Grumman and Douglas
Lunar Saturn IB
Saturn V
3 3.91 5,500 CM + 14,700 LM
24,500 Service Module
Fuel cells 1967 1975 15 (4)[note 1]
Gemini  USA McDonnell Aircraft
Martin
LEO Titan II GLV
Titan IIIC[note 2]
2 5.56 3.05 Fuel cells 1965 1966 10 (2)[note 1]
Mercury  USA McDonnell Aircraft
North American Aviation
LEO
attained
Redstone MRLV
Atlas LV-3B
1 3.34 1.89 Batteries 1961 1963 6 (12)[note 1]
Shenzhou  China LEO Chang Zheng 2F 3 9.25 2.80 7,840 Solar panels 1,450 2003 Active 5 (5)
Soyuz 7K-OK  USSR OKB-1 LEO Soyuz 3 7.48 2.72 Solar panels 1967 1970 8 (8)[note 3]
Soyuz 7KT-OK  USSR OKB-1 LEO Soyuz 3 7.48 2.72 Solar panels 1971 1971 2[note 4]
Soyuz 7K-T  USSR OKB-1 LEO Soyuz
Soyuz-U
2 7.48 2.72 Batteries 1973 1981 26 (4)[note 5]
Soyuz 7K-T-AF  USSR OKB-1 LEO Soyuz 2 7.48 2.72 Solar panels 1973 1973 1
Soyuz 7K-TM  USSR OKB-1 LEO Soyuz-U 2 7.48 2.72 Solar panels 1974 1975 2 (2)
Soyuz 7K-MF6  USSR OKB-1 LEO Soyuz-U 2 7.48 2.72 Solar panels 1976 1976 1
Soyuz-T  USSR OKB-1 LEO Soyuz-U
Soyuz-U2
3 7.48 2.72 Solar panels 1978 1986 15 (6)[note 6]
Soyuz-TM  USSR
 Russia
RKK Energia LEO Soyuz-U2
Soyuz-U
3 7.48 2.72 Solar panels 1986 2002 33 (1)
Soyuz-TMA
11F732
 Russia RKK Energia LEO Soyuz-FG 3 7.48 2.72 Solar panels 2002 2012 22
Soyuz TMA-M
11F747
 Russia RKK Energia LEO Soyuz-FG 3 7.48 2.72 7,150 Solar panels 1,000 2010 2016 13
Soyuz TMA-MS
?
 Russia RKK Energia LEO Soyuz-FG 3 Solar panels 2016
Biconic Space Vehicle  USA Blue Origin LEO Orbital Reusable Booster System
CST-100  USA Boeing LEO multiple, initially Atlas V 7 [1] 5.03 m [2] 4.56 m [2]
Dream Chaser  USA Sierra Nevada Corporation LEO multiple, initially Atlas V 7 [3][4] 9.0 m [5] 11,300 kg [6]
PPTS
?
 Russia RKK Energia LEO Solar panels 2018 or later
Voskhod  USSR OKB-1 LEO Voskhod 3[note 7] 5 2.4 Batteries n/a 1964 1965 2 (3)
Vostok  USSR OKB-1 LEO
first
Vostok-K 1 4.4 2.43 4,725 Batteries n/a 1961 1963 6 (7)[note 8]
SpaceShipOne  USA Scaled Composites 112 km
X Prize
White Knight
Hybrid Motor
3 3,600 2004 2004 3[note 9]
Space Shuttle orbiter  USA United Space Alliance LEO Space Shuttle 8[note 10] 109,000 Fuel cells 1981 2011 135[note 11]
X-15  USA North American Aviation 108 km
altitude
B-52
Ammonia-LOX
1 15,420 1963 1963 2[note 12]
Orion  USA Lockheed Martin
Astrium
Mars Delta IV Heavy
Space Launch System
4 5 8,900 Capsule
12,300 Service Module
Solar Panels 2014 or later 0[note 13]
Dragon V2  USA SpaceX LEO Falcon 9 7[note 14] 3.7 Solar Panels 2015 or later 0[note 15]
SpaceShipTwo  USA The Spaceship Company 110 km
Kármán line+10
White Knight Two
RocketMotorTwo
8[note 16] 9,740 2014 0[note 17]
* - Format: Manned (Unmanned), includes failures

Footnotes

  1. 1.0 1.1 1.2 Not including Boilerplate tests
  2. One unmanned launch on Titan IIIC ahead of proposed use in MOL programme
  3. Manned flights include one fatal in-flight failure; Soyuz 1 lost due to parachute failure upon landing.
  4. Manned flights include one fatal in-flight failure; Soyuz 11 depressurised during reentry.
  5. Manned flights include one launch failure - abort during third stage flight, recovered after suborbital flight
  6. Manned flights include one launch failure (SAS (launch escape system) used ~70 seconds before planned liftoff due to fire on launch pad - crew survived)
  7. Able to carry three cosmonauts without spacesuits, or two with spacesuits; both combinations flown
  8. Unmanned flight count includes two launch failures
  9. Does not include manned atmospheric flights
  10. No missions carried more than eight astronauts, although higher crew sizes were theoretically possible, for example recovering the crew of a stranded orbiter.
  11. Includes two fatal accidents; STS-51-L disintegrated during ascent, STS-107 damaged during ascent, disintegrated during reentry.
  12. Does not include atmospheric flights, or missions considered spaceflights by the US definition but not the internationally-accepted definition
  13. Did not include unmanned test around 2014
  14. Number of seats will probably be a multiple of the 3 crew member rotations for the ISS
  15. This is SpaceX's advertised Goal. Did not find NASA schedule.
  16. 2 crew + 6 passengers
  17. Does not include manned atmospheric flights

See also

References

  1. "Commercial Human Spaceflight Plan Unveiled". Aviation Week. July 20, 2010. Retrieved September 16, 2010.
  2. 2.0 2.1 Burghardt, Mike (August 2011). "Boeing CST-100: Commercial Crew Transportation System". Boeing. Retrieved May 8, 2014.
  3. "Dream Chaser Model Drops in at NASA Dryden" (Press release). Dryden Flight Research Center: NASA. 2010-12-17. Archived from the original on 2014-01-07. Retrieved 2012-08-29.
  4. Chang, Kenneth (2011-02-01). "Businesses Take Flight, With Help From NASA". New York Times. p. D1. Archived from the original on 2014-01-06. Retrieved 2012-08-29.
  5. Wade, Mark (2014). "Dream Chaser". Encyclopedia Astronautix. Archived from the original on 2014-01-06. Retrieved 2012-08-29.
  6. Sirangelo, Mark (August 2011). "NewSpace 2011: Sierra Nevada Corporation". Spacevidcast. Retrieved 2011-08-16. Sirangelo, Mark (24 August 2014). "Flight Plans and Crews for Commercial Dream Chaser’s First Flights: One-on-One Interview With SNC VP Mark Sirangelo (Part 3)". AmericaSpace.