Falcon-1

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Falcon-1 [SpaceX]

Falcon-1 is a small liquid fueled orbital launch vehicle, which was developed by SpaceX (Space Exploration Technologies Corp.). Both stages are Kerosene / LOX fueled.

The first stage, which will be reusable after recovery by parachutes, is powered by the SpaceX built Merlin engine. The second stage is be propelled by the Kestrel engine, which uses technology derived from the of the Lunar Module Descent Engine.

Launch sites are SLC-3W at Vandenberg for high inclination launches and a launch site on Omelek Island in the Marshall Islands. A Cape Canaveral launch pad is also considered for launching tonto low inclination orbits.

The basic Falcon-1 vehicle carries up to 420 kg payloads to low equatorial earth orbit. SpaceX claims, the Falcon will reduce the costs for an orbital launch by the factor of three - a price of $ 6.7 million for the basic version is planned.

The operational Falcon-1 uses the regeneratively cooled Merlin-1C engine beginning with the third Falcon flight in mid 2008 in contrast to the ablatively cooled Merlin-1A of the Falcon-1 development version.

→ List of all Falcon-1 flights

No.  TypNo Type             Date          LS           Payload 

 3    1    Falcon-1         03.08.2008 F  Om           Trailblazer / PreSat / Nanosail D / Celestis 07
 4    2    Falcon-1         28.09.2008    Om           Ratsat
 5    3    Falcon-1         14.07.2009    Om           RazakSat 1
 
 
Failures:
 3: Stage separation failure


Launch Sites

Om    Omelek Island, Kwajalein, Marshall Islands
Va    Vandenberg SLC-3W (not used)