Comparison of space station cargo vehicles

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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
TKS  Soviet Union Proton-K 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-2.1a 7.2 7,150 2,230 Operational[2]
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
Dragon  USA SpaceX Falcon 9 6.1 4,200[5] 10,200 3,310 pressurized or unpressurized, in any mixture[6] 10.0 (pressurized), plus 14 (unpressurized), or 34 (unpressurized with extended trunk)[7] 2,500 capsule return[8] 3.7 2,000[9] Operational
Dragon V2 cargo  USA SpaceX Falcon 9 Development
HTV  Japan JAXA H-IIB 10 10,500[10] 16,500[10] 6,000[10] 14 (pressurized, plus 16 unpressurized)[11] None 4.4 Operational
HTV-X  Japan JAXA H3 Launch Vehicle[12] None Development
Cygnus (standard)  USA Orbital Antares 5.14 1,500[13] 2,000[13] 18.9[13] None 3.07 3,500[14] Retired
Cygnus (enhanced)  USA Orbital ATK Antares
Atlas V 401
6.34 1,800[15] 2,700[15] 27[15] None 3.07 Operational
Dream Chaser Cargo System  USA Sierra Nevada Corporation Atlas V 5,000 pressurized, 500 unpressurized[16] 1,750[16] Development

See also

References

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  7. http://www.spacex.com/downloads/dragonlab-datasheet.pdf
  8. http://www.nasaspaceflight.com/2012/10/falcon-9loft-dragon-crs-1-mission-iss-attempt1/
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