FORMAT: 1A
HOST: https://api.spacexdata.com/v2/
Endpoints allowing you to get information related to SpaceX capsules.
Home | Launches | Rockets | Capsules | Company Info | Parts | Launchpads
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Response 200 (application/json)
[ { "id": "dragon1", "name": "Dragon 1", "type": "capsule", "active": true, "crew_capacity": 0, "sidewall_angle_deg": 15, "orbit_duration_yr": 2, "heat_shield": { "material": "PICA-X", "size_meters": 3.6, "temp_degrees": 3000, "dev_partner": "NASA" }, "thrusters": [ { "type": "Draco", "amount": 18, "pods": 4, "fuel_1": "nitrogen tetroxide", "fuel_2": "monomethylhydrazine", "thrust": { "kN": 0.4, "lbf": 90 } } ], "launch_payload_mass": { "kg": 6000, "lb": 13228 }, "launch_payload_vol": { "cubic_meters": 25, "cubic_feet": 883 }, "return_payload_mass": { "kg": 3000, "lb": 6614 }, "return_payload_vol": { "cubic_meters": 11, "cubic_feet": 388 }, "pressurized_capsule": { "payload_volume": { "cubic_meters": 11, "cubic_feet": 388 } }, "trunk": { "trunk_volume": { "cubic_meters": 14, "cubic_feet": 494 }, "cargo": { "solar_array": 2, "unpressurized_cargo": true } }, "height_w_trunk": { "meters": 7.2, "feet": 23.6 }, "diameter": { "meters": 3.7, "feet": 12 }, "wikipedia": "https://en.wikipedia.org/wiki/SpaceX_Dragon", "description": "Dragon is a reusable spacecraft developed by SpaceX, an American private space transportation company based in Hawthorne, California. Dragon is launched into space by the SpaceX Falcon 9 two-stage-to-orbit launch vehicle. The Dragon spacecraft was originally designed for human travel, but so far has only been used to deliver cargo to the International Space Station (ISS)." }, ]
- Parameters
- capsule_id (string) - ID of the capsule
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Response 200 (application/json)
{ "id": "dragon2", "name": "Dragon 2", "type": "capsule", "active": false, "crew_capacity": 0, "sidewall_angle_deg": 15, "orbit_duration_yr": 2, "heat_shield": { "material": "PICA-X", "size_meters": 3.6, "temp_degrees": 3000, "dev_partner": "NASA" }, "thrusters": [ { "type": "Draco", "amount": 18, "pods": 4, "fuel_1": "nitrogen tetroxide", "fuel_2": "monomethylhydrazine", "thrust": { "kN": 0.4, "lbf": 90 } } ], "launch_payload_mass": { "kg": 6000, "lb": 13228 }, "launch_payload_vol": { "cubic_meters": 25, "cubic_feet": 883 }, "return_payload_mass": { "kg": 3000, "lb": 6614 }, "return_payload_vol": { "cubic_meters": 11, "cubic_feet": 388 }, "pressurized_capsule": { "payload_volume": { "cubic_meters": 11, "cubic_feet": 388 } }, "trunk": { "trunk_volume": { "cubic_meters": 14, "cubic_feet": 494 }, "cargo": { "solar_array": 2, "unpressurized_cargo": true } }, "height_w_trunk": { "meters": 7.2, "feet": 23.6 }, "diameter": { "meters": 3.7, "feet": 12 } }