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Come back daily for more porn always free and fresh right at your fingertips. TNAFlix is the 1 porn site with videos to feed your porn crave. Get in on some hot free porn action at TNAFlix pumping out fresh porn since 2. Falcon 1 Wikipedia. Falcon 1. Falcon 1 rocket. Function. Orbital launch vehicle. Manufacturer. Space. XCountry of origin. United States. Project cost. US9. 0 million. Size. Height. 21. 3 m 7. Diameter. 1. 7 m 5. Mass. 38,5. 55 kg 8. Stages. 2Capacity. Payload to LEO1. 80 kg 4. Payload to. SSO4. Launch history. Status. Retired2Launch sites. Omelek Island. Total launches. Successes. 2Failures. Partial failures. First flight. March 2. GMTLast flight. July 1. GMTFirst stage. Engines. Merlin 1. A first 2 flights, 1 Merlin 1. C final 3 flightsThrust. N 1. 02,0. 00 lbfSpecific impulse. NskgBurn time. Fuel. RP 1LOXSecond stage. Engines. 1 Kestrel. Thrust. 31 k. N 7,0. Specific impulse. NskgBurn time. Fuel. RP 1LOXThe Falcon 1 was an expendable launch systemprivatelydeveloped and manufactured by Space. X during 2. 00. 62. On 2. 8 September 2. Falcon 1 became the first privately developed liquid fuel launch vehicle to go into orbit around the Earth. The two stage to orbitrocket used LOXRP 1 for both stages, the first powered by a single Merlin engine and the second powered by a single Kestrel engine. It was designed by Space. X from the ground up. The vehicle was launched a total of five times. Falcon 1 achieved orbit on its fourth attempt, in September 2. On 1. 4 July 2. 00. Falcon 1 made its final flight and successfully delivered the Malaysian. Razak. SAT satellite to orbit on Space. Xs first commercial launch fifth launch overall. Following its fifth launch, the Falcon 1 was retired and succeeded by Falcon 9. Space. X had announced an enhanced variant, the Falcon 1e,2 but development was stopped in favor of Falcon 9. HistoryeditPrivate fundingeditThe Falcon 1 rocket was developed with private funding. The only other orbital launch vehicles to be privately funded and developed were the Conestoga in 1. Pegasus, first launched in 1. The total development cost of Falcon 1 was approximately US9. While the development of Falcon 1 was privately funded, the first two Falcon 1 launches were purchased by the United States Department of Defense under a program that evaluates new US launch vehicles suitable for use by DARPA. Launches previously planned, but never flown on Falcon 1editAs part of a US1. Falcon 1 was to carry the Tac. Bridge Commander Maximum Warp Edition more. Sat 11. 1 in 2. By late May 2. Space. X stated that Falcon 1 was ready to launch Tac. Sat 1 from Vandenberg. But the Air Force did not want the launch of an untested rocket to occur until the final Titan IV flew from nearby SLC 4. E. Subsequent and repeated delays due to Falcon 1 launch failures delayed Tac. Sat 1s launch. After Tac. Sat 2 was launched on an Orbital Sciences Minotaur I on December 1. Department of Defense re evaluated the need for launching Tac. Sat 1. In August 2. Department of Defense canceled the planned launch of Tac. Sat 11. 2 because all of the Tac. Sat objectives had been met. An August 2. 00. 5 update on Space. Xs website 1. 3 showed 6 launches planned for Falcon 1, with customers including MDA Corp CASSIOPE, which eventually launched in 2. Falcon 9, Swedish Space Corp and US Air Force. First stage view of the Merlin engine. According to Space. X, the Falcon 1 was designed to minimize price per launch for low Earth orbitsatellites, increase reliability, and optimize flight environment and time to launch. It also was used to verify components and structural design concepts that would be reused in the Falcon 9. Space. X started with the smallest useful orbital rocket Falcon 1 with about 1. First stageeditThe first stage was made from friction stir welded. It employs a common bulkhead between the LOX and RP 1 tanks, as well as flight pressure stabilization. It can be transported safely without pressurization like the heavier Delta II isogrid design but gains additional strength when pressurized for flight like the Atlas II, which could not be transported unpressurized. The parachute system, built by Irvin Parachute Corporation, uses a high speed drogue chute and a main chute. For the first two launches, the Falcon 1 used a Merlin 1. A engine. An improved version of the Merlin 1. A, the Merlin 1. B, was supposed to fly on later flights of the Falcon 1, although it was further improved to create the Merlin 1. C, which was first flown on the third Falcon 1 flight, and on the first 5 flights of the Falcon 9. The Falcon 1 first stage was powered by a single pump fed. Merlin 1. C engine burning RP 1 and liquid oxygen providing 4. Isp 2. 90 s. 1. 6 The first stage burns to depletion, taking around 1. Second stageeditThe second stage Falcon 1 tanks were built with a cryogenic compatible 2. Falcon 1e. 1. 6 The helium pressurization system pumps propellant to the engine, supplies heated1. The Kestrel engine includes a titanium heat exchanger to pass waste heat to the helium, thereby greatly extending its work capacity. The pressure tanks are composite overwrapped pressure vessels made by Arde corporation with inconel alloy and are the same as those used in the Delta IV. The second stage was powered by a pressure fed. Kestrel engine with 3. ReusabilityeditThe first stage was originally planned to return by parachute to a water landing and be recovered for reuse, but this capability was never demonstrated. The second stage was not designed to be reusable. Launch sequenceeditAt launch, the first stage engine Merlin is ignited and throttled to full power while the launcher is restrained and all systems are verified by the flight computer. If the systems are operating correctly, the rocket is released and clears the tower in about seven seconds. The first stage burn lasts about 2 minutes and 4. Stage separation is accomplished with explosive bolts and a pneumatically actuated pusher system. The second stage Kestrel engine burns for about six minutes, inserting the payload into a low Earth orbit. It is capable of multiple restarts. PricingeditSpace. X is one of the few launch system operators that publishes its launch prices, which are quoted as being the same for all customers. In 2. 00. 5 Falcon 1 was advertised as costing 5. In 2. 00. 6 until 2. In late 2. 00. 9 Space. X announced new prices for the Falcon 1 and 1e at 7 million and 8. Falcon 1 and 1e would fly as secondary payloads on the Falcon 9. Historically, the Falcon 1 was originally planned to launch about 6. Earth orbit for US6,0. US9,0. 00,0. 00. It was Space. Xs offering intended to open up the smallsatlaunch market to competition. The final version of the Falcon 1, the Falcon 1e,2. US1. 1 million. The vehicle is now retired. Several years ago, Space. X was going to open up the smallsat launch market with the Falcon 1, which originally was to launch about 6. LEO for 6 million the payload capacity later declined to about 4. Later, the Falcon 1e was to provide approximately 1,0. Launch sitesedit. Falcon 1 first flight attempt with NASA partnership cargo at Omelek Island launchpad. All flights have been launched from Kwajalein Atoll using the Space. X launch facility on Omelek Island and range facilities of the Reagan Test Site. Vandenberg AFB Space Launch Complex 3. W was the original launch site for Falcon 1, but it was abandoned at the test fire stage due to persistent schedule conflicts with adjacent launch pads. Cape Canaveral Air Force Station Space Launch Complex 4. Falcon 9 pad was considered for Falcon 1 launches but never developed before Falcon 1 was retired. VariantseditLaunch historyeditFalcon 1 made five launches.