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Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/SpaceX_reusable_launch_system_development_program> ?p ?o }

• SpaceX_reusable_launch_system_development_program abstract "The SpaceX reusable launch system development program is a privately funded program to develop a set of new technologies for an orbital launch system that may be reused many times in a manner similar to the reusability of aircraft. The company SpaceX is developing the technologies over a number of years to facilitate full and rapid reusability of space launch vehicles. The project's long-term objectives include returning a launch vehicle first stage to the launch site in minutes and to return a second stage to the launch pad following orbital realignment with the launch site and atmospheric reentry in up to 24 hours. Both stages will be designed to allow reuse a few hours after return.The program was publicly announced in 2011 and the design for returning the rocket to its launchpad using only its own propulsion systems was completed in February 2012. SpaceX's active test program began in late 2012 with testing low-altitude, low-speed aspects of the landing technology. High-velocity, high-altitude aspects of the booster atmospheric return technology began testing in late 2013.The reusable launch system technology is under development for the first stages of the Falcon family of rockets. It is particularly well-suited to the Falcon Heavy where the two outer cores separate from the rocket earlier in the flight, and are therefore moving more slowly at stage separation. If the technology is used on a reusable Falcon 9 rocket, the first-stage separation would occur at a velocity of approximately 2.0 km/s (6,500 km/h; 4,100 mph; Mach 6) rather than the 3.4 km/s (11,000 km/h; 7,000 mph; Mach 10) for an expendable Falcon 9, to provide the residual fuel necessary for the deceleration and turnaround maneuver and the controlled descent and landing. The reusable technology will also be extended to both the first and upper stages of the future launch vehicle for the Mars Colonial Transporter.The first successful controlled landing of an orbital rocket stage on the ocean surface was achieved in April 2014. Two of the controlled-descent tests have also attempted to land the returning first stage on a floating landing platform—one each in January and April 2015. But although the booster was guided to the floating platform in both cases, neither test was successful in achieving a vertical landing on the platform.".
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• SpaceX_reusable_launch_system_development_program wikiPageWikiLink Grasshopper_(rocket).
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• SpaceX_reusable_launch_system_development_program wikiPageWikiLink LOX.
• SpaceX_reusable_launch_system_development_program wikiPageWikiLink Landing_ellipse.
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• SpaceX_reusable_launch_system_development_program wikiPageWikiLink Landing_gear.
• SpaceX_reusable_launch_system_development_program wikiPageWikiLink Launch_pad.
• SpaceX_reusable_launch_system_development_program wikiPageWikiLink Launch_vehicle.
• SpaceX_reusable_launch_system_development_program wikiPageWikiLink Launch_vehicle_landing_gear.
• SpaceX_reusable_launch_system_development_program wikiPageWikiLink Lift_(force).

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