Specs for the next-gen Falcon 9 v. 1.1 and Falcon Heavy are in.
Merlin 1D
(Current Merlin 1C: 95,000 lbf & 125,000 lbf)
Merlin 1D sea level thrust: 147,000 lbf (1st stage)
Merlin 1D sea level ISP: 282 seconds
Merlin 1DVac vacuum thrust: 161,000 lbf (second stage)
Merlin 1DVac vacuum ISP: 311 seconds
Falcon 9 v. 1.1
(Falcon 9 1.0: 47.85 m / 157 ft w/Dragon)
Overall length: 69.2 m (227 ft)
Width: 3.6 m (12 ft)
Engines: 9x Merlin 1D + 1x Merlin 1DVac
Total thrust (sea level): 5.88 MN (1,320,000 lbf)
Mass to Low Earth Orbit (LEO): 13,150 kg (29,000 lb)
Mass to Geosynchronous Transfer Orbit (GTO): 4,850 kg (10,692 lb)
Falcon Heavy
Overall length: 69.2 m (227 ft)
Width: 3.6 m (12 ft) x 11.6 m (38 ft)
Engines: 27x Merlin 1D + 1x Merlin 1DVac
Total thrust: 17 MN (3,800,000 lbf)
Mass to Low Earth Orbit (LEO): 53,000 kg (117,000 lb)
Mass to Geosynchronous Transfer Orbit (GTO): 12,000 kg (26,460 lb)
Rumored (strongly): an advanced staged combustion engine that could increase the above payloads significantly.
Dragon will be available with 2 sizes of cargo trunk; the existing 2.3 meter long version and a 4.3 meter long version for larger unpressurized cargo.
Falcon 9 v. 1.0 is the one used for flight 3, the last ISS mission. The F9 v. 1.1 goes live with flight 6, and will be used for both cargo and the DragonRider crewed flights. It also serves as the core stage for Falcon Heavy, and its first stage is used as the side boosters for FH.
Falcon Heavy will come in 2 configurations: one using fuel / liquid oxygen cross-feed and one not.
When using cross-feed extra fuel and liquid oxygen are pumped from the side boosters into the core stage so that when the side boosters separate the core stage has full tanks, increasing the mass to orbit. Technically, this makes Falcon Heavy a 2.5 stage rocket. Non-cross-feed would be used for smaller than max payloads and will be cheaper.
SpaceX has signed a major deal with Intelsat, the worlds largest operator of communications satellites, to launch large satellites on the Falcon Heavy.
They have also signed a deal with SpaceFlight Services to provide secondary, micro and mini satellite launches. Their deployment bus will be mounted on top of the second stage, then after the main payload (ex: Dragon or a large satellite) is deployed the second stage will re-light to put the other payloads into their orbits.
SpaceFlight Services will also handle payloads for the DragonLab free-flying experiment platform - an uncrewed robotic Dragon capable of 2 year science etc. missions. This will open up long term ISS-style microgravity research to universities, companies & governments who can't get ISS time.
DragonLab PDF....
SpaceFlight Services payload bus
Falcon variants
Merlin 1D
(Current Merlin 1C: 95,000 lbf & 125,000 lbf)
Merlin 1D sea level thrust: 147,000 lbf (1st stage)
Merlin 1D sea level ISP: 282 seconds
Merlin 1DVac vacuum thrust: 161,000 lbf (second stage)
Merlin 1DVac vacuum ISP: 311 seconds
Falcon 9 v. 1.1
(Falcon 9 1.0: 47.85 m / 157 ft w/Dragon)
Overall length: 69.2 m (227 ft)
Width: 3.6 m (12 ft)
Engines: 9x Merlin 1D + 1x Merlin 1DVac
Total thrust (sea level): 5.88 MN (1,320,000 lbf)
Mass to Low Earth Orbit (LEO): 13,150 kg (29,000 lb)
Mass to Geosynchronous Transfer Orbit (GTO): 4,850 kg (10,692 lb)
Falcon Heavy
Overall length: 69.2 m (227 ft)
Width: 3.6 m (12 ft) x 11.6 m (38 ft)
Engines: 27x Merlin 1D + 1x Merlin 1DVac
Total thrust: 17 MN (3,800,000 lbf)
Mass to Low Earth Orbit (LEO): 53,000 kg (117,000 lb)
Mass to Geosynchronous Transfer Orbit (GTO): 12,000 kg (26,460 lb)
Rumored (strongly): an advanced staged combustion engine that could increase the above payloads significantly.
Dragon will be available with 2 sizes of cargo trunk; the existing 2.3 meter long version and a 4.3 meter long version for larger unpressurized cargo.
Falcon 9 v. 1.0 is the one used for flight 3, the last ISS mission. The F9 v. 1.1 goes live with flight 6, and will be used for both cargo and the DragonRider crewed flights. It also serves as the core stage for Falcon Heavy, and its first stage is used as the side boosters for FH.
Falcon Heavy will come in 2 configurations: one using fuel / liquid oxygen cross-feed and one not.
When using cross-feed extra fuel and liquid oxygen are pumped from the side boosters into the core stage so that when the side boosters separate the core stage has full tanks, increasing the mass to orbit. Technically, this makes Falcon Heavy a 2.5 stage rocket. Non-cross-feed would be used for smaller than max payloads and will be cheaper.
SpaceX has signed a major deal with Intelsat, the worlds largest operator of communications satellites, to launch large satellites on the Falcon Heavy.
They have also signed a deal with SpaceFlight Services to provide secondary, micro and mini satellite launches. Their deployment bus will be mounted on top of the second stage, then after the main payload (ex: Dragon or a large satellite) is deployed the second stage will re-light to put the other payloads into their orbits.
SpaceFlight Services will also handle payloads for the DragonLab free-flying experiment platform - an uncrewed robotic Dragon capable of 2 year science etc. missions. This will open up long term ISS-style microgravity research to universities, companies & governments who can't get ISS time.
DragonLab PDF....
SpaceFlight Services payload bus
Falcon variants
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