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Por ejemplo, un Delta 7925 tiene la tercera fase anterior, nueve propulsores GEM, y una tercera fase PAM. Un Delta 7320 es un vehículo con dos fases y 3 cohetes propulsores sólidos. Un Delta II-Heavy (Pesado) tiene los propusores GEM-46, más grandes, diseñados originariamente para el Delta III .
Delta II was an expendable launch system, originally designed and built by McDonnell Douglas, and sometimes known as the Thorad Delta 1. Delta II was part of the Delta rocket family, derived directly from the Delta 3000, and entered service in 1989.
Delta II: creado en 1989 para sustituir al vetusto Delta I, el Delta II fue un cohete de lo más fiable para la NASA. Existen diferentes versiones como el nuevo 7925 o el 7925-Heavy. Delta III: nacido en 1998, el enorme cohete ofrece el doble de capacidad de carga que su predecesor, pero fue un total fracaso tras no ejecutar ni un vuelo exitoso.
A Delta II solid rocket booster (SRB) GPS IIR-1 was launched on a Delta II 7925-9.5 launch vehicle, serial number D241, from Launch Complex 17A (LC-17A) at the Cape Canaveral Air Force Station (CCAFS). The launch occurred at 16:28:01 UTC, on 17 January 1997.
Sun. The two STEREO spacecraft were launched at 00:52 UTC on October 26, 2006, from Launch Pad 17B at the Cape Canaveral Air Force Station in Florida on a Delta II 7925-10L launcher into highly elliptical geocentric orbits. The apogee reached the Moon's orbit.
Delta II was an expendable launch system, originally designed and built by McDonnell Douglas. Delta II was part of the Delta rocket family and entered service in 1989. Delta II vehicles included the Delta 6000, and the two later Delta 7000 variants ("Lite" and "Heavy").
The Delta II is an expendable launch, medium-lift vehicle used to launch Global Positioning System satellites into orbit, providing navigational data to military users. Additionally, the Delta II launches civil and commercial payloads into low-earth, polar, geosynchronous transfer and stationary orbits. Features.
