There are 26 images added between 20 November 2006 and 8 November 2010
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Delta II  
Initial Operational Capability (IOC): 1989
Total Production: 111
Origin: United States of America
Corporations: Boeing
Parent System: Delta
Initial Operational Capability (IOC): 1960
Total Production: 304
Family Members: Delta III and Delta IV
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Description: The Delta expendable launch vehicle program started in 1959 to meet the requirements of NASA. The Delta I launch vehicle propulsion system took its first stage from the USAF's Thor Intermediate Range Ballistic Missile (IRBM) and the second stage from the US Navy's Vanguard ballistic missile. In 1960 the first Delta I vehicle was capable of delivery a 100-pound payload into the GTO (Geosynchronous Transfer Orbit).

The US Air Force started the Delta II program in 1987 to put into orbit 18 NAVSTAR GPS satellites. The success of the GPS system increased the number of Delta II launch vehicles ordered by the USAF and therefore the success of the Delta II program.

The propulsion system can be configured with two or three stages (typically one RS-27 and two LR-101 for the first stage, one AJ10 motor for the second stage and one Star-48B for the optional third stage) plus 3, 4 or 9 GEM boosters depending on mission needs. Payloads of up to 4,750 lb (2,142 kg) can be put into the GTO and loads of up to 13,280 lb (6,000 kg) into low Earth orbit.

Currently, the Delta II launch vehicle is employed to put into orbit GPS satellites, as well as commercial and civil payloads into low-Earth, polar, GTO and stationary orbits.

Delta II Specifications

Crew: 0
Number of Stages: 3
Dimensions
Height: 38.3 meter (1,509 inch)
Rocket Diameter: 2.40 meter
Weight
Max Lift-off Thrust: 699,250 pound (317 ton)
Max Lift-off Weight: 232 ton (511,177 pound)
Payload to GTO: 2,142 kilogram (4,722 pound)
Payload to LEO: 6,000 kilogram (13,228 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Delta II News

There are 9 news between
17 Nov 2006 and 24 Oct 2008
Friday, October 24, 2008Boeing Launches Third Italian Earth Observation Satellite
Saturday, March 15, 2008US Air Force 6th Modernized GPS Satellite Successfully Launched from Cape Canaveral
Friday, December 21, 2007Delta II Rocket with GPS Block IIR-M Payload Successfully Launches
Saturday, December 8, 2007Delta II Rocket Launches Second Italian COSMO-SkyMed Satellite
Wednesday, October 17, 2007US Air Force Launches Fourth GPS Block IIR-M Satellite
Thursday, September 20, 2007Boeing Awarded Launch Services Contract for Third COSMO-SkyMed Satellite
Friday, June 8, 2007Boeing Delta II Successfully Launches First COSMO-SkyMed Spacecraft
Tuesday, December 19, 2006Delta II Rocket Successfully Carries National Reconnaissance Office Payload Into Space
Friday, November 17, 2006Delta II Rocket Delivers GPS IIR-16(M) Into Orbit

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
GEM 40x9
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