Falcon 1 Data Sheet â SCM 2008-006 - FOIA and eLibrary website!
Falcon 1 Data Sheet â SCM 2008-006 - FOIA and eLibrary website!
Falcon 1 Data Sheet â SCM 2008-006 - FOIA and eLibrary website!
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<strong>Falcon</strong> 1 <strong>Data</strong> <strong>Sheet</strong> – <strong>SCM</strong> <strong>2008</strong>‐<strong>006</strong>
<strong>Falcon</strong> 1<strong>Falcon</strong> 1 <strong>Data</strong> <strong>Sheet</strong> – <strong>SCM</strong> <strong>2008</strong>‐<strong>006</strong>SpaceX recognizes that nothing is more important than getting our customer’s spacecraft safely to its intendeddestination. <strong>Falcon</strong> 1 launch vehicles are designed to provide breakthrough advances in reliability, cost, <strong>and</strong>time to launch. The primary design driver is <strong>and</strong> will remain reliability.The <strong>Falcon</strong> 1 launch vehicle offers the lowest price launch on the market, <strong>and</strong> it has been the pathfinder for allsubsequent SpaceX launch vehicles. The <strong>Falcon</strong> 1 User’s Guide outlines the environments <strong>and</strong> structuralcharacteristics of the launch vehicle in detail. The st<strong>and</strong>ard <strong>Falcon</strong> 1 will be available for launches untilmid 2010, upon which time the upgraded <strong>Falcon</strong> 1e will become the vehicle for transporting smallpayloads. <strong>Falcon</strong> 1e is the next generation of the <strong>Falcon</strong> 1 launch vehicle <strong>and</strong> offers additionalcapability enabled by an upgraded Merlin engine,elongated first stage tank, <strong>and</strong> an exp<strong>and</strong>ed fairing.<strong>Falcon</strong> 1<strong>Falcon</strong> 1eLength 21.3 m (70 ft) 27.4 m (90 ft)Width 1.7 m (5.5 ft) 1.7 m (5.5 ft)Mass 27,670 kg (61,000 lbs) 46,760 kg (103,000 lbs)Thrust at liftoff 347 kN (78,000 lbf) 556 kN (125,000 lbf)Mass to LEO 420 kg (926 lb) 1010 kg (2220 lb)Price* $7.9 M $9.1 M*US dollars paid‐in‐full at Authority‐to‐Proceed, January 1, <strong>2008</strong>.Direct & Two‐burn Performance, 9.1° InclinationTwo‐burn Performance to LEOPayload Mass (kg)11002400100022009002000800180070016<strong>006</strong>001400120050010004008003<strong>006</strong>00200400100200000 500 1000 1500 2000 2500 3000 3500Payload Mass (lbm)Payload Mass (kg)110010009008007<strong>006</strong>0050040030020010000 20 40 60 80 100240022002000180016001400120010008<strong>006</strong>004002000Payload Mass (lbm)Orbit Altitude (km)Inclination (deg)<strong>Falcon</strong> 1e ‐ Two Burn Insertion<strong>Falcon</strong> 1e ‐ Direct Insertion<strong>Falcon</strong> 1 ‐ Two Burn Insertion<strong>Falcon</strong> 1 ‐ Direct Insertion<strong>Falcon</strong> 1e ‐ 185 km<strong>Falcon</strong> 1e ‐ 300 km<strong>Falcon</strong> 1e ‐ 500 km<strong>Falcon</strong> 1e ‐ 700 km<strong>Falcon</strong> 1 ‐ 185 km<strong>Falcon</strong> 1 ‐ 300 km<strong>Falcon</strong> 1 ‐ 500 km<strong>Falcon</strong> 1 ‐ 700 km