Delta II

**Delta II** was a rocket used to launch various projects into space. The Delta series of rockets were first designed and made by McDonnell Douglas. This company joined with Boeing in 1997. Delta II rockets had been made since 2006 by United Launch Alliance, which is a joint company owned by Boeing and Lockheed Martin to supply launch rockets to the US government. Boeing Launch Services supplied Delta II rockets to private companies.

The Delta II rockets were based on the Thor rockets built in the 1950's. These were first made to be intercontinental ballistic missiles. The first Thor was launched on January 26, 1957. The Delta II rocket was first launched on 14 February 1989. The rocket was developed after the explosion of the  in 1986. The US Air Force needed another way to launch its GPS satellites. As of 2018, there had been 156 Delta II launches from both Cape Canaveral Air Force Station and the Vandenberg Air Force Base. Only two launches were unsuccessful. On 5 August 1995, a rocket motor failure meant the Koreasat 1 was put into a lower orbit. On 17 January 1997, Delta 241 carrying the GPS IIR-1 exploded 13 seconds after taking off.

The last time the Delta II took off on 15 September 2018, when she carried the ICESat-2 satellite.

## Related pages

- Delta IV

## Infobox (rocket/payload)

- **location**: Low Earth orbit, LEO


## Infobox (rocket/payload)

- **location**: Geostationary transfer orbit, GTO


## Infobox (rocket/payload)

- **location**: Heliocentric orbit, HCO


## Infobox (rocket/stage)

- **type**: booster
- **diff**: 6000 Series
- **name**: Castor 4A
- **number**: 9
- **engines**: Solid
- **solid**: yes
- **burntime**: 56 s
- **propellant**: Aluminum fuel, ammonium perchlorate oxidizer in an HTPB binder


## Infobox (rocket/stage)

- **type**: booster
- **diff**: 7000 Series
- **name**: Graphite-Epoxy Motor, GEM 40
- **number**: 3, 4, or 9
- **engines**: Solid
- **solid**: yes
- **burntime**: 64 s
- **propellant**: Aluminum fuel, ammonium perchlorate oxidizer in an HTPB binder


## Infobox (rocket/stage)

- **type**: booster
- **diff**: 7000 Heavy
- **name**: Graphite-Epoxy Motor, GEM 46
- **number**: 9
- **engines**: Solid
- **solid**: yes
- **burntime**: 75 s
- **propellant**: Aluminum fuel, ammonium perchlorate oxidizer in an HTPB binder


## Infobox (rocket/stage)

- **type**: stage
- **stageno**: First
- **name**: Thor/Delta XLT(-C)
- **engines**: 1 RS-27 (6000 series) or RS-27A (7000 series)
- **burntime**: 265 s
- **fuel**: LOX/RP-1


## Infobox (rocket/stage)

- **type**: stage
- **stageno**: Second
- **name**: Delta K
- **engines**: 1 AJ-10, AJ10-118K
- **burntime**: 431 s
- **fuel**: / Aerozine 50


## Infobox (rocket/stage)

- **type**: stage
- **stageno**: Third
- **name**: Payload Assist Module, PAM-D (optional)
- **engines**: Star 48B
- **solid**: yes
- **burntime**: 87 s
- **propellant**: Aluminum fuel, ammonium perchlorate oxidizer in an HTPB binder


## Infobox (rocket)

- **image**: Delta II Genesis Launch.jpg
- **caption**: A Delta II rocket takes off from Cape Canaveral Air Force Station, Cape Canaveral
- **name**: Delta II
- **function**: Launch vehicle
- **manufacturer**: United Launch Alliance
- **country-origin**: United States
- **cpl**: in 1987 (7920-10 mod.)
- **stages**: 2 or 3
- **status**: Retired
- **sites**: Cape Canaveral Air Force Station, Cape Canaveral Cape Canaveral Air Force Station Space Launch Complex 17, SLC-17
Vandenberg AFB Vandenberg AFB Space Launch Complex 2, SLC-2W
- **launches**: 156
**Delta 6000:** 17
**Delta 7000:** 132
**Delta 7000H:** 6
- **success**: 154
**Delta 6000:** 17
**Delta 7000:** 130
**Delta 7000H:** 6
- **fail**: 1 (Delta 7000)
- **partial**: 1 (Delta 7000)