Engineering:Comparison of crewed space vehicles
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A number of different spacecraft have been used to carry people to and from outer space.
Table code key
Spacecraft under development | |
Spacecraft is operational | |
Retired spacecraft | |
Payload To / From the ISS | |
§ | Crewed (Uncrewed) [Includes failures] |
Orbital and interplanetary space vehicles
Spacecraft | Origin | Manufacturer | Range | Launch system | Crew size | Length (m) | Diameter (m) | Launch mass (kg) | Power system | Payload (kg) | First spaceflight § | Last spaceflight | Flights § |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Mercury | USA | McDonnell Aircraft North American Aviation |
LEO attained |
Redstone MRLV Atlas LV-3B |
1 | 3.34 | 1.89 | 1,400 | Batteries | 1961 (1960) | 1963 | 6 (12)[note 1] | |
Gemini | USA | McDonnell Aircraft Martin |
LEO | Titan II GLV Titan IIIC[note 2] |
2 | 5.56 | 3.05 | 3,790 | Fuel cells | 1965 (1964) | 1966 | 10 (2)[note 3] | |
Apollo | USA | North American Aviation Grumman and Douglas |
Lunar | Saturn IB Saturn V |
3 | 8.5 | 3.91 | 5,500 CM + 14,700 LM + 24,500 Service Module |
Fuel cells | 1967 (1966) | 1975 | 15 (4)[note 3] | |
Space Shuttle orbiter | USA | Rockwell International | LEO | Space Shuttle | 8[note 4] | 37.24 | 4.8[note 5] | 109,000 | Fuel cells | 12,500/16,000 | 1981 | 2011 | 135[note 6] |
Soyuz 7K-T | Soviet Union | OKB-1 | LEO | Soyuz Soyuz-U |
2 | 7.48 | 2.72 | Batteries | 1973 | 1981 | 26 (4)[note 7] | ||
Voskhod | Soviet Union | OKB-1 | LEO | Voskhod | 3[note 8] | 5 | 2.4 | 5,682 | Batteries | 1964 (1964) | 1965 | 2 (3) | |
Vostok | Soviet Union | OKB-1 | LEO first |
Vostok-K | 1 | 4.4 | 2.43 | 4,725 | Batteries | 1961 (1960) | 1963 | 6 (7)[note 9] | |
Soyuz 7K-OK | Soviet Union | OKB-1 | LEO | Soyuz | 3 | 7.48 | 2.72 | Solar panels | 1967 (1966) | 1970 | 8 (8)[note 10] | ||
Soyuz 7KT-OK | Soviet Union | OKB-1 | LEO | Soyuz | 3 | 7.48 | 2.72 | Solar panels | 1971 | 1971 | 2[note 11] | ||
Soyuz 7K-T-AF | Soviet Union | OKB-1 | LEO | Soyuz | 2 | 7.48 | 2.72 | Solar panels | 1973 | 1973 | 1 | ||
Soyuz 7K-TM | Soviet Union | OKB-1 | LEO | Soyuz-U | 2 | 7.48 | 2.72 | Solar panels | 1974 | 1975 | 2 (2) | ||
Soyuz 7K-MF6 | Soviet Union | OKB-1 | LEO | Soyuz-U | 2 | 7.48 | 2.72 | Solar panels | 1976 | 1976 | 1 | ||
Soyuz-T | Soviet Union | OKB-1 | LEO | Soyuz-U Soyuz-U2 |
3 | 7.48 | 2.72 | Solar panels | 1978 | 1986 | 15 (6)[note 12] | ||
Soyuz-TM | Soviet Union Russia |
RKK Energia | LEO | Soyuz-U2 Soyuz-U |
3 | 7.48 | 2.72 | Solar panels | 1986 | 2002 | 33 (1) | ||
Buran | Soviet Union | RKK Energia | LEO | Energia | 10 | 36.37 | Fuel cells | N/A (1988) | (1988) | 0 (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 | 2010 | 2016 | 19 | |
Shenzhou | China | China Academy of Space Technology | LEO | Chang Zheng 2F | 3 | 9.25 | 2.80 | 7,840 | Solar panels | 2003 (1999) | Active | 12 (5) | |
Soyuz MS |
Russia | RKK Energia | LEO | Soyuz-2.1a | 3 | 7.48 | 2.72 | Solar panels | 2016 | Active | 22 (2) | ||
Crew Dragon | USA | SpaceX | LEO | Falcon 9 | 4[1] | 8.1[2] | 3.7[3] | 12,055[4] | Solar Panels | 3,307/2,507 | 2020 (2019) | Active | 11 (1) |
CST-100 Starliner | USA | Boeing | LEO | Atlas V | 7 [note 13][5] | 5.03 [6] | 4.56 [6] | Solar panels | 2024 (2019) | Testing | 0 (2) | ||
Orion | USA | Lockheed Martin Astrium |
Lunar, Mars | Space Launch System | 6 | 3.3 | 5 | 8,900 capsule + 12,300 service module |
Solar panels | 2025 (2014) | Testing | 0 (2)[note 14] | |
Next-gen crewed spacecraft | China | China Aerospace Science and Technology Corporation | LEO, Lunar | Long March 10 | 7 | 8.8 | 4.5 | 21,600 | Solar panels | 2026 (2020) | Testing | 0 (1) | |
Gaganyaan | India | Indian Space Research Organization | LEO | GSLV Mk III | 3 | 7 | 3.5 | 7,800 | Solar Panels | (Planned: 2024) | Planned | 0 | |
Starship | USA | SpaceX | Solar System[7][note 15] | Super Heavy | 100 [note 16] | 55 [7] | 9 [7][note 17] | 1,335,000 [7] | Solar Panels | (Planned: 2023) [7] | Testing | 0 | |
Orel |
Russia | RKK Energia | LEO,Lunar | Irtysh (rocket) Angara A5 |
4 | Solar panels | (Planned: 2028) | Planned | 0 | ||||
Dream Chaser | USA | Sierra Nevada Corporation | LEO | Vulcan Centaur | 7 [8][9] | 9 [10] | 11,300 [11] | TBA | Planned | 0 | |||
Biconic Space Vehicle | USA | Blue Origin | LEO | New Glenn | TBA | Planned | 0 | ||||||
Nyx | Germany France | The Exploration Company | LEO,Lunar | TBA | Planned | 0 |
Suborbital space vehicles
Spacecraft | Origin | Manufacturer | Altitude | Launch system | Crew size | Length (m) | Diameter (m) | Launch mass (kg) | Power system | Generated power (W) | First spaceflight § | Last spaceflight | Flights § |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
SpaceShipOne | USA | Scaled Composites | 112 km X Prize |
White Knight Hybrid Motor |
1 | 8.53 | 8.05 | 3,600 | 2004 | 2004 | 3[note 18] | ||
X-15 | USA | North American Aviation | 108 km altitude |
B-52 Ammonia-LOX |
1 | 15.45 | 6.8 | 15,420 | 1963[note 19] | 1963 | 2[note 20] | ||
SpaceShipTwo | USA | Virgin Galactic | 90 km | White Knight Two RocketMotorTwo |
8[note 21] | 18.3 | 8.3 | 9,740 | December 13, 2018 | 2[note 22] | |||
New Shepard | USA | Blue Origin | 119 km | New Shepard BE-3 |
6 | 2021 (2015) |
6 (17) | ||||||
Spica Rocket | Denmark | Copenhagen Suborbitals | 105 km | BPM100 | 1 | 13 | 1 | 4,100 | Batteries | 2025 | Early Development | 0 | |
SpaceShipThree | USA | Virgin Galactic | Approximately 90 km | White Knight Two | 8[note 23] | 18.3 | 8.3 | 9,740 | Unknown | Undergoing initial ground testing | 0[note 24] |
Footnotes
- ↑ Including 2 suborbital flights, not including boilerplate tests
- ↑ One uncrewed launch on Titan IIIC ahead of proposed use in MOL programme
- ↑ 3.0 3.1 Not including boilerplate tests
- ↑ No missions carried more than eight astronauts, although higher crew sizes were theoretically possible, for example recovering the crew of a stranded orbiter.
- ↑ Wingspan 23.79m
- ↑ Includes two fatal accidents; STS-51-L disintegrated during ascent, STS-107 damaged during ascent, disintegrated during reentry.
- ↑ Crewed flights include one launch failure - abort during third stage flight, recovered after suborbital flight
- ↑ Able to carry three cosmonauts without spacesuits, or two with spacesuits; both combinations flown
- ↑ Uncrewed flight count includes two launch failures
- ↑ Crewed flights include one fatal in-flight failure; Soyuz 1 lost due to parachute failure upon landing.
- ↑ Crewed flights include one fatal in-flight failure; Soyuz 11 depressurised during reentry.
- ↑ Crewed flights include one launch failure (SAS (launch escape system) used ~70 seconds before planned liftoff due to fire on launch pad - crew survived)
- ↑ Each mission in the Commercial Crew Program will send up to four astronauts to the ISS
- ↑ Including uncrewed test in 2014
- ↑ Designed to land almost everywhere in the solar system
- ↑ Number of seats will be lower on early missions
- ↑ Plus delta wings
- ↑ Does not include crewed atmospheric flights
- ↑ Does not include only-U.S.-recognized spaceflights
- ↑ Does not include atmospheric flights, or missions considered spaceflights by the US definition but not the FAI's definition
- ↑ 2 crew + 6 passengers
- ↑ Does not include crewed atmospheric flights
- ↑ 2 crew + 6 passengers
- ↑ Does not include crewed atmospheric flights
See also
- Cargo spacecraft (robotic resupply spacecraft)
- Comparison of orbital launch systems
- Comparison of orbital rocket engines
- Comparison of space station cargo vehicles
- Human spaceflight
References
- ↑ Clark, Stephen (7 December 2019). "After redesigns, the finish line is in sight for SpaceX's Crew Dragon spaceship". Spaceflight Now. https://spaceflightnow.com/2019/12/07/after-redesigns-the-finish-line-is-in-sight-for-spacexs-crew-dragon/. "'With [the addition of parachutes] and the angle of the seats, we could not get seven anymore', Shotwell said. "So now we only have four seats. That was kind of a big change for us"."
- ↑ "Falcon 9". SpaceX. https://www.spacex.com/falcon9.
- ↑ "SpaceX Brochure – 2008". https://www.spacex.com/SpaceX_Brochure_V7_All.pdf.
- ↑ Clark, Stephen. "SpaceX's Crew Dragon ready for first test flight – Spaceflight Now" (in en-US). https://spaceflightnow.com/2019/02/28/spacexs-crew-dragon-rolls-out-for-test-flight/.
- ↑ Reichhardt, Tony (August 2018). "Astronauts, Your Ride's Here!". https://www.airspacemag.com/space/space-series-starliner-and-spacex-dragon-180969499/.
- ↑ 6.0 6.1 Burghardt, Mike (August 2011). "Boeing CST-100: Commercial Crew Transportation System". Boeing. http://www.boeing.com/assets/pdf/defense-space/space/ccts/docs/CCDev2%20Boeing%20CST-100%20Overview.pdf.
- ↑ 7.0 7.1 7.2 7.3 7.4 "Making Life Multiplanetary". SpaceX. 2017-10-18. http://www.spacex.com/sites/spacex/files/making_life_multiplanetary-2017.pdf.
- ↑ "Dream Chaser Model Drops in at NASA Dryden" (Press release). Dryden Flight Research Center: NASA. 2010-12-17. Archived from the original on 2012-06-12. Retrieved 2012-08-29.
- ↑ Chang, Kenneth (2011-02-01). "Businesses Take Flight, With Help From NASA". New York Times: p. D1. https://www.nytimes.com/2011/02/01/science/space/01private.html?_r=4&ref=science&pagewanted=all.
- ↑ Wade, Mark (2014). "Dream Chaser". Encyclopedia Astronautix. http://www.astronautix.com/craft/drehaser.htm.
- ↑ Sirangelo, Mark (August 2011). "NewSpace 2011: Sierra Nevada Corporation". Spacevidcast. https://www.youtube.com/watch?v=D7sWtEAddkM. 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. https://www.americaspace.com/2014/08/23/flight-plans-and-crews-for-commercial-dream-chasers-first-flights-one-on-one-interview-with-snc-vp-mark-sirangelo-part-3/.
Original source: https://en.wikipedia.org/wiki/Comparison of crewed space vehicles.
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