Falcon 9
Falcon 9 is a two stage medium lift launch Vehicle Designed and manufactured by space. It is the first orbital class lift launch vehicle to reflight. Falcon 9 can Launch up to 22,800 kg to LEO (low Earth orbit) and 8,300 kg to GTO (geostationary transfer orbit).
Function - medium lift launch vehicle
Manufacturer - space x
Country of origin - United States
Height
v1.2 - 70 m
v1.1 - 68.4 m
v1.0 - 54.9 m
Diameter - 3.6 m
Stages - 2
Payload to LEO
v1.2 - 22,800 kg
v1.1 - 13,150 kg
v1.0 - 10.450 kg
Payload to GTO
v1.2 - 8,300 kg
v1.1 - 4,850 kg
v1.0 - 4,540 kg
First stage
Engine
v1.2 - 9 Merlin 1D +
v1.1 - 9 Merlin 1D
v1.0 - 9 Merlin 1C
Thrust
v1.2 - 7,607 kn
v1.1 - 5,885 kn
v1.0 - 4,940 kn
Burn time
v1.2 - 162 seconds
v1.1 - 180 seconds
v1.0 - 170 seconds
Fuel - LOX/RP-1
Second stage
Engine
v1.2 - 1 Merlin 1D vacuum+
v1.1 - 1 Merlin 1D vacuum
v1.0 - 1 Merlin 1C vacuum
Thrust
v1.2 - 934 kn
v1.1 - 801 kn
v1.0 - 617 kn
Burn time
v1.2 - 397 seconds
v1.1 - 375 seconds
v1.0 - 345 seconds
Fuel - LOX/RP-1
Source : spacex |
Profile
Function - medium lift launch vehicle
Manufacturer - space x
Country of origin - United States
Height
v1.2 - 70 m
v1.1 - 68.4 m
v1.0 - 54.9 m
Diameter - 3.6 m
Stages - 2
Payload to LEO
v1.2 - 22,800 kg
v1.1 - 13,150 kg
v1.0 - 10.450 kg
Payload to GTO
v1.2 - 8,300 kg
v1.1 - 4,850 kg
v1.0 - 4,540 kg
First stage
Engine
v1.2 - 9 Merlin 1D +
v1.1 - 9 Merlin 1D
v1.0 - 9 Merlin 1C
Thrust
v1.2 - 7,607 kn
v1.1 - 5,885 kn
v1.0 - 4,940 kn
Burn time
v1.2 - 162 seconds
v1.1 - 180 seconds
v1.0 - 170 seconds
Fuel - LOX/RP-1
Second stage
Engine
v1.2 - 1 Merlin 1D vacuum+
v1.1 - 1 Merlin 1D vacuum
v1.0 - 1 Merlin 1C vacuum
Thrust
v1.2 - 934 kn
v1.1 - 801 kn
v1.0 - 617 kn
Burn time
v1.2 - 397 seconds
v1.1 - 375 seconds
v1.0 - 345 seconds
Fuel - LOX/RP-1
Comments
Post a Comment