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EntityQ49538· pop 40· linked from 721 articles

Also known as Delta 6000, Delta 7000

retired expendable launch system in the Delta rocket family

Key facts

Function
Launch vehicle
Manufacturer
McDonnell Douglas , (1989–1997) Boeing Defense, Space & Security (1997–2006) United Launch Alliance (2006–2018)
Country of origin
United States
Cost per launch
US$51 million in 1987 US$137 million in 2018
Height
38.9 m (128 ft)
Diameter
2.44 m (8 ft)
Mass
152,000–286,100 kg (335,100–630,700 lb)
Orbital inclination
28.7°
Status
Retired
Launch sites
Cape Canaveral , SLC-17 Vandenberg , SLC-2W
Total launches
155: Delta 6000: 17 Delta 7000: 132 Delta 7000 Heavy: 6
Success es
153: Delta 6000: 17 Delta 7000: 130 Delta 7000 Heavy: 6
Failure
1 (Delta 7000)
Partial failure
1 (Delta 7000)
First flight
Delta 6000: 14 February 1989 ( USA-35 ) Delta 7000: 26 November 1990 ( USA-66 ) Delta 7000 Heavy: 7 July 2003 ( Opportunity rover )
Last flight
Delta 6000: 24 July 1992 ( Geotail ) Delta 7000: 15 September 2018 ( ICESat-2 ) Delta 7000 Heavy: 10 September 2011 ( GRAIL )
Empty mass
1,457 kg (3,212 lb)
Gross mass
11,578 kg (25,525 lb)

via Wikipedia infobox

Wikidata facts

Image
Delta II Dawn liftoff 1.jpg
Show 3 more facts
first flight
1989-02-14
Commons category
Delta II
Commons gallery
Delta (rocket)
Sources (2)

via Wikidata · CC0

~19 min read

Article

Delta II was an expendable launch system designed and built by McDonnell Douglas, sometimes known as the Thorad Delta 1. Delta II was part of the Delta rocket family, derived from the Delta 3000, and entered service in 1989. There were two main variants, the Delta 6000 and Delta 7000, with the latter also having "Light" and "Heavy" subvariants. During its career, Delta II flew several payloads, including 24 Global Positioning System (GPS) Block II satellites, several dozen NASA payloads, and 60 Iridium communication satellites. The rocket flew its final mission, ICESat-2, on 15 September 2018, earning a streak of 100 consecutive successful missions, with the last failure being GPS IIR-1 in 1997. In the late 1990s, Delta II was developed into the unsuccessful Delta III, which was in turn developed into the more capable and successful Delta IV, though the latter shares little heritage with the original Thor and Delta rockets.

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