Falcon-Heavy [SpaceX]
Falcon-9 is a liquid fueled orbital launch vehicle for medium to heavy sized missions, which is currently under development at SpaceX (Space Exploration Technologies Corp.). It is techonologically based on the Falcon-1 launch vehicle. Both stages are Kerosene / LOX fueled.
The first stage, which will be reusable after recovery by parachutes, is to be powered by 9 of the SpaceX built Merlin-1C engines with regenerative cooling. The upper stage will use a single Merlin engine and will also be reusable. The Falcon-Heavy is offered with a 5.2 m fairing.
Planned launch site is Cape Canaveral launch pad (SLC-40) for low inclination launches.
The first flight for a Falcon-Heavy is planned for 2013.
| Version | Strap-On | Stage 1 | Stage 2 |
|---|---|---|---|
| Falcon-Heavy | 2 x Stage 1 (str.) / 9 Merlin-1D | Stage 1 (str.) / 9 Merlin-1D | Stage 2 / 1 Merlin-Vac |
| Performance (kg) | LEO | LPEO | SSO | GTO | GEO | MolO | IP |
|---|---|---|---|---|---|---|---|
| Falcon-Heavy | 53000 | 19500 | - | - |
No. TypNo Type Date LS Payload
None
planned launches
1 Falcon-Heavy xx.xx.2013 Va SLC-4E ?
Launch Sites
CC Cape Canaveral, SLC-40
Va Vandenberg SLC-3W