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- 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.
www.vandenberg.spaceforce.mil › About-Us › Fact-Sheets
The Delta II launch vehicle offered the user a choice of three fairings: a 2.9-m (9.5-ft)-diameter skin-and-stringer center section fairing (bisector), and two versions of a 3-m (10-ft)-diameter (bisector) composite fairing with two different lengths.
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.
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.
This document contains current Delta II information and includes United Launch Alliance plans and projections for Delta II launch services launch vehicle specifications. Included are Delta II family vehicle descriptions, target vehicle performance figures, payload envelopes, an-
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The Delta II expendable launch vehicle is the product of a long evolution that dates back to the earliest days of American missile development. Use of proven components and gradual modification of those components has resulted in one of the most reliable launch vehicles in the world.
The Delta II launch vehicle offers the user a choice of three fairings: a 2.9-m (9.5-ft)-diameter skin-and-stringer center section fairing (bisector), and two versions of a 3-m (10-ft)-diameter (bisector) composite fairing with two different lengths.
Nov 26, 1990 · Delta II 7000 Series Launch, Photo Courtesy NASA. Classification: Space Launch Vehicle. Length: 128 feet. Diameter: 8 feet. Date of First Cape Canaveral Launch: November 26, 1990. Date of Final Cape Canaveral Launch: September 10, 2011. Number of Cape Canaveral Launches: 94. The Delta II 7000 Series improved performance by employing new solid ...
