Comparison of space station cargo vehicles
A number of different spacecraft have been used to carry cargo to and from space stations.
Legend for below table: [under development] — [retired,canceled] — [operational,inactive]
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) | Status |
---|---|---|---|---|---|---|---|---|---|---|---|---|
Progress 7K-TG | Soviet Union | Energia | Soyuz-U | None | Retired | |||||||
Progress-M 11F615A55 |
Soviet Union Russia |
Energia | Soyuz-U Soyuz-U2 |
7.2 | 7,130 | 2,600 | 7.6 | 150 with optional Raduga capsule | 2.72 | 600[1] | Retired | |
Progress-M1 |
Russia | Energia | Soyuz-U Soyuz-FG |
None | Retired | |||||||
Progress-M 11F615A60 |
Russia | Energia | Soyuz-U Soyuz-2.1a |
7.2 | 7,150 | 2,230 | 7.6 | None | 2.72 | 700 | Retired | |
Progress-MS | Russia | Energia | Soyuz-U Soyuz-2.1a |
7.2 | 7,150 | 2,230 | Operational[2] | |||||
TKS | Soviet Union | TsKBM | Proton-K | Retired | ||||||||
ATV | Europe | EADS | Ariane 5ES | 10.3 | 10,470[3] | 20,750[3] | 7,667[3] | 48 (pressurized) | None | 4.5 | 3,800[4] | Retired |
HTV | Japan | JAXA | H-IIB | 10 | 10,500[5] | 16,500[5] | 4,500 pressurized, 1,500 unpressurized[5] | 14 (pressurized), plus 16 (unpressurized)[6] | 20 with optional capsule[7] | 4.4 | Operational | |
HTV-X | Japan | JAXA | H3 Launch Vehicle[8] | 5,200 pressurized, 2,000 unpressurized[9] | 78[9] | Development | ||||||
Dragon | USA | SpaceX | Falcon 9 | 6.1 | 4,200[10] | 10,200 | 3,310 pressurized or unpressurized, in any mixture[11] | 10.0 (pressurized), plus 14 (unpressurized), or 34 (unpressurized with extended trunk)[12] | 2,500 capsule return[13] | 3.7 | 2,000[14] | Operational |
Dragon 2 cargo | USA | SpaceX | Falcon 9 | 8.1 | 6,400 | 3,310 | 10.0 (pressurized), plus 14 (unpressurized) | 2,500 | 3.7 | Development | ||
Cygnus (standard) | USA | Orbital | Antares 1x0 | 5.14 | 1,500[15] | 2,000[15] | 18.9[15] | None | 3.07 | 3,500[16] | Retired | |
Cygnus (enhanced) | USA | Orbital ATK | Antares 230 Atlas V 401 |
6.34 | 1,800[17] | 3,500[17] | 27[17] | None | 3.07 | Operational | ||
Tianzhou | China | CAST | Long March 7 | 9 | 13,500 | 6,500 includes 2,000 propellant | 3.35 | Operational | ||||
Dream Chaser Cargo System | USA | Sierra Nevada Corporation | Atlas V Vulcan[18] |
5,000 pressurized, 500 unpressurized[19] | 1,750[19] | Development |
See also
- Comparison of manned space vehicles
- Comparison of orbital launch systems
- Comparison of orbital rocket engines
- Automated cargo spacecraft
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.
- 1 2 3 "ESA Automated Transfer Vehicle". ESA. Retrieved 7 August 2013.
- ↑ "ATV Utilization Relevant Data" (PDF). Retrieved 29 May 2012.
- 1 2 3 "JAXA H-II Transfer Vehicle (HTV) Overview". JAXA. Retrieved 7 August 2013.
- ↑ "JAXA H-II Transfer Vehicle (HTV)" (PDF). NASA. Retrieved 10 January 2014.
- ↑ "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.
- 1 2 "HTV-Xの開発状況について" (PDF) (in Japanese). Japan Aerospace Exploration Agency. 14 July 2016. Retrieved 2016-07-15.
- ↑ "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.
- 1 2 3 "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.
- 1 2 3 "Cygnus Spacecraft Information". Spaceflight101.
- ↑ "NSRC Day 2 Summary". Parabolic Arc. Retrieved 6 June 2016.
- 1 2 "Sierra Nevada Hopes Dream Chaser Finds "Sweet Spot" of ISS Cargo Competition". SpaceNews. Retrieved 20 February 2016.
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