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As of 2015, the most recent Pegasus XL to be purchased — a planned June 2017 launch of NASA's Ionospheric Connection Explorer (ICON) mission — had a total cost of US$56.3 million, which NASA notes includes "firm-fixed launch service costs, spacecraft processing, payload integration, tracking, data and telemetry and other launch support ...
The first Pegasus launch to use Stargazer was conducted on June 27, 1994, as the maiden flight of the Pegasus-XL. Previous launches used the NASA-operated Boeing B-52 nicknamed "Balls 8," which was also used for four subsequent launches, as the original Pegasus could not be launched from Stargazer due to clearance issues. A modified version ...
Launch Date Mission Vehicle Launch Site Total Launch Cost* (million) 1998 [3] 1998.10.24 Deep Space 1: Delta II 7326-9.5 Cape Canaveral Air Force Station Space Launch Complex 17 (CCAFS SLC 17A) 1998.12.06 Submillimeter Wave Astronomy Satellite (SWAS) Pegasus XL: Vandenberg Air Force Base (VAFB) 1998.12.11 Mars Climate Orbiter: Delta II 7425
The article is organized into two tables: the first contains a list of currently active and under-development launcher families, while the second contains a list of retired launcher families. The related article " Comparison of orbital launch systems " lists each individual launcher system within any given launcher family, categorized by its ...
Expendable launch vehicles can accommodate all types of orbit inclinations and altitudes and are ideal vehicles for launching Earth-orbit and interplanetary missions. The Launch Services Program was established at Kennedy Space Center for NASA's acquisition and program management of expendable launch vehicle missions.
The launch system would consist of three primary components: a carrier aircraft, contracted to Scaled Composites; a launch vehicle, originally contracted to SpaceX as a derivative of the Falcon 9 [8] —later contracted to Orbital Sciences as the Pegasus II; and a mating and integration system to enable the aircraft to safely interface with ...
Now known as the Medium Launch Vehicle, or MLV, the rocket is now 4.32 m (14.17 ft) in diameter with 7 Miranda engines on the first stage and 1 Vira engine on the second stage. [52] It will be capable of delivering over 16,000 kg to LEO in a 5 m (16.4 ft) fairing. [ 53 ]
Launch of CYGNSS on a Pegasus-XL. The CYGNSS mission was launched on December 15, 2016, at 13:37:21 UTC from a single Pegasus XL air-launched rocket. The rocket was deployed from a customized Lockheed L-1011 aircraft, Orbital ATK 's Stargazer, from a position 201 kilometers (125 mi) off the coast of Cape Canaveral, Florida.