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| [
{
"id": "dragon1",
"name": "Dragon 1",
"type": "capsule",
"active": true,
"crew_capacity": 0,
"sidewall_angle_deg": 15,
"orbit_duration_yr": 2,
"dry_mass_kg": 4200,
"dry_mass_lb": 9300,
"first_flight": "2010-12-8",
"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)."
},
{
"id": "dragon2",
"name": "Dragon 2",
"type": "capsule",
"active": false,
"crew_capacity": 7,
"sidewall_angle_deg": 15,
"orbit_duration_yr": 2,
"dry_mass_kg": 6350,
"dry_mass_lb": 14000,
"first_flight": null,
"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
}
},
{
"type": "SuperDraco",
"amount": 8,
"pods": 4,
"fuel_1": "dinitrogen tetroxide",
"fuel_2": "monomethylhydrazine",
"thrust": {
"kN": 71,
"lbf": 16000
}
}
],
"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/Dragon_2",
"description": "Dragon 2 (also Crew Dragon, Dragon V2, or formerly DragonRider) is the second version of the SpaceX Dragon spacecraft, which will be a human-rated vehicle. It includes a set of four side-mounted thruster pods with two SuperDraco engines each, which can serve as a launch escape system or launch abort system (LAS). In addition, it has much larger windows, new flight computers and avionics, and redesigned solar arrays, and a modified outer mold line from the initial cargo Dragon that has been flying for several years."
}
]
|
