Comparison of space station cargo vehicles
A number of different spacecraft have been used to carry cargo to and from space stations.
Under development; Operational or inactive; Retired or canceled;
Spacecraft | Origin | Manufacturer | Launch system | Length (m) | Dry mass (kg) | Launch mass (kg) | Payload (kg) | Payload volume (m3) | Return payload (kg) | Diameter (m) | Generated power (W) | Automated docking | Status (no. of flights) |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Progress 7K-TG | Energia | Soyuz-U | None | No | Retired (43) | ||||||||
Progress-M 11F615A55 |
Energia | Soyuz-U Soyuz-U2 |
7.2 | 7,130 | 2,600 | 7.6 | 150, with optional Raduga capsule | 2.72 | 600[1] | Yes | Retired (66) | ||
Progress-M1 |
Energia | Soyuz-U Soyuz-FG |
None | Yes | Retired (11) | ||||||||
Progress-M 11F615A60 |
Energia | Soyuz-U Soyuz-2.1a |
7.2 | 7,150 | 2,230 | 7.6 | None | 2.72 | 700 | Yes | Retired (27 + 2 failed) | ||
Progress-MS | Energia | Soyuz-U Soyuz-2.1a |
7.2 | 7,150 | 2,230 | None | Yes | Operational[2] | |||||
Soyuz GVK | Energia | Soyuz-2.1b | 7.23 | 8,020 | 1,966 | 500 | 2.72 | Yes | Development[3] | ||||
TKS | TsKBM | Proton-K | 17.51 | 13,688 | 21,620 | 12,600 | 4.15 | 2,400 | No | Retired (4) | |||
ATV | EADS | Ariane 5ES | 10.3 | 10,470[4] | 20,750[4] | 7,667[4] | 48, pressurized | None | 4.5 | 3,800[5] | Yes | Retired (5) | |
HTV | JAXA | H-IIB | 10 | 10,500[6] | 16,500[6] | 3,000, pressurized; 1,000, unpressurized[6] | 14, pressurized; 16, unpressurized[6] | 20, with optional HSRC[7] | 4.4 | 200 | No | Operational | |
HTV-X | JAXA | H3 Launch Vehicle[8] | 10 with cargo module, 6.2 without | 8,300 | 15,500, combined[9] | 4,069, pressurized; optional 1,750, unpressurized | 78, combined | 4.4 | 1,000 | No, technology trial of an automated IDSS docking port fitted in place of unpressurised cargo module being planned | Development | ||
Dragon | SpaceX | Falcon 9 | 6.1 | 4,200[10] | 10,200 | 6,000, in any combination of pressurized or unpressurized[11] | 10.0, pressurized; 14, unpressurized; 34, unpressurized with extended trunk[12] | 3,000, capsule return[13] | 3.7 | 2,000[14] | No | Retired (19 + 1 failed)[15] | |
Dragon 2 cargo | SpaceX | Falcon 9 | 8.1 | 6,400 | 6,000[16] | 9.3, pressurized, return volume; 37, unpressurized |
3,000[17] | 4.0 | Yes | Operational | |||
Cygnus (standard) | Orbital | Antares 1x0 | 5.14 | 1,500[18] | 2,000[18] | 18.9[18] | None | 3.07 | 3,500[19] | No | Retired (3 + 1 failed) | ||
Cygnus (enhanced) | Northrop Grumman | Antares 230 Antares 230+ Atlas V 401 |
6.34 | 1,800[20] | 3,500[20] | 27[20] | None | 3.07 | No | Operational | |||
Tianzhou | CAST | Long March 7 | 9 | 13,500 | 6,500, incl. 2,000 propellant | None | 3.35 | Yes | Operational | ||||
Dream Chaser Cargo System | Sierra Nevada Corporation | Atlas V Vulcan[21] |
5,000, pressurized; 500, unpressurized[22] | 1,750[22] | Yes | Development | |||||||
Starship cargo | SpaceX | Super Heavy | 50[23] | 120,000 (target)[24] | 1,320,000[25] | 150,000 (target)[26] | 9[23] | Unknown | Development |
See also
References
- "Progress M". Archived from the original on 3 August 2009. Retrieved 29 May 2012.
- "Upgraded Progress MS docks with the ISS". NASASpaceflight.com. 23 December 2015. Retrieved 26 December 2015.
- "Retrievable Soyuz GVK spacecraft". RussianSpaceWeb. Retrieved 24 January 2019.
- "ESA Automated Transfer Vehicle". ESA. Retrieved 7 August 2013.
- "ATV Utilization Relevant Data" (PDF). Retrieved 29 May 2012.
- "JAXA transition examination of the new space station supply machine (HTV-X)" (PDF). JAXA. Retrieved 6 February 2018.
- "HTV 搭載小型回収カプセルの開発" (PDF) (in Japanese). Japan Aerospace Exploration Agency. 12 November 2014. Retrieved 2016-10-21.
- "H3,H‐IIA/Bのミッション割当て(案)" (PDF) (in Japanese). MEXT. 8 March 2016. Retrieved 2016-03-10.
- http://www.jaxa.jp/press/2017/12/files/20171206_HTV-X.pdf
- "SpaceX Brochure v7" (PDF). Archived from the original (PDF) on 20 March 2012. Retrieved 29 May 2012.
- Bergin, Chris (19 October 2012). "Dragon enjoying ISS stay, despite minor issues – Falcon 9 investigation begins". NASASpaceflight.com. Retrieved 21 October 2012.
CRS-2 will debut the use of Dragon’s Trunk section, capable of delivering unpressurized cargo, prior to the payload being removed by the ISS’ robotic assets after berthing.
- http://www.spacex.com/sites/spacex/files/pdf/DragonLabFactSheet.pdf
- http://www.nasaspaceflight.com/2012/10/falcon-9loft-dragon-crs-1-mission-iss-attempt1/
- "Dragonlab Datasheet" (PDF). Archived from the original (PDF) on 4 January 2011. Retrieved 29 May 2012.
- Clark, Stephen. "With successful splashdown, SpaceX retires first version of Dragon spacecraft – Spaceflight Now". Retrieved 2020-04-10.
- "Dragon". SpaceX. Retrieved 11 April 2020.
- "Dragon". SpaceX. Retrieved 11 April 2020.
- "Cygnus Fast Sheet" (PDF). Orbital Sciences Co. Retrieved 7 August 2013.
- "The Annual Compendium of Commercial Space Transportation: 2012" (PDF). Federal Aviation Administration. February 2012. Retrieved 8 February 2013.
- "Cygnus Spacecraft Information". Spaceflight101.
- "NSRC Day 2 Summary". Parabolic Arc. Retrieved 6 June 2016.
- "Sierra Nevada Hopes Dream Chaser Finds "Sweet Spot" of ISS Cargo Competition". SpaceNews. Retrieved 20 February 2016.
- "Starship". SpaceX. Retrieved 2 October 2019.
- Elon Musk (28 September 2019). Starship Update (video). SpaceX. Event occurs at 1:45. Retrieved 30 September 2019 – via YouTube.
- Elon Musk on Twitter: 3 sea level optimized Raptors, 3 vacuum optimized Raptors (big nozzle)
- Elon Musk on Twitter: 150mT for reference payload compared to other rockets.
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