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Delta 5000

Series of American expendable launch systems


Series of American expendable launch systems

FieldValue
nameDelta 5000 series
imageCOBELaunch.jpg
captionLaunch of the Delta 5920 with COBE
functionExpendable launch system
country-originUnited States
cplin 1985
alt-cplin 2018
height34 m
diameter2.44 m
mass201,580 kg
stages2
sitesVandenberg SLC-2W
launches1
success1
statusRetired
only18 November 1989
locationLEO
kilos3848 kg
locationGTO
kilos1405 kg
familyDelta
comparableDelta 4000, Delta II
stagedata
typebooster
diff
stageno
nameCastor 4A
number9
length9.12 m
diameter1.02 m
width
empty1,529 kg
gross11,743 kg
propmass
enginesSolid
solidyes
thrust478.3 kN
total
SI{{plainlist
burntime56 s
propellantAluminum fuel, ammonium perchlorate oxidizer in an HTPB binder
typestage
diff
stagenoFirst
nameThor/Delta ELT
number
length22.37 m
diameter2.44 m
width
empty4,360 kg
gross84,368 kg
propmass
engines1 RS-27
solid
thrust1030.2 kN
total
SI{{plainlist
burntime223 s
fuelLOX / RP-1
typestage
diff
stagenoSecond
nameDelta K
number
length5.89 m
diameter2.44 m
width
empty950 kg
gross6,954 kg
propmass
engines1 AJ10-118K
solid
thrust43.6 kN
total
SI319 s
burntime431 s
fuel/ Aerozine 50

|country-origin = United States |alt-cpl = in 2018

  • Sea level: 237 seconds
  • Vacuum: 266 seconds
  • Sea level: 262 seconds
  • Vacuum: 296 seconds

The Delta 5000 series was an American expendable launch system which was used to conduct an orbital launch in 1989. It was a member of the Delta family of rockets. Although several variants were put forward, only the Delta 5920 was launched. The designation used a four digit numerical code to store information on the configuration of the rocket. It was built from a combination of spare parts left over from earlier Delta rockets, which were being retired, and parts from the Delta II 6000-series, which was just entering service.

The first stage was the RS-27 powered Extended Long Tank Thor, flown on several earlier Delta rockets. Nine Castor-4A solid rocket boosters were attached to increase thrust at lift-off, replacing the less powerful Castor-4 boosters used on the 3000 series. The Delta-K was used as a second stage. In the configuration that was launched, no third stage was flown.

The Delta 5000 was launched just once, from Space Launch Complex 2W at the Vandenberg Air Force Base. Launch occurred at 14:34 on 18 November 1989. It was successful, and placed the Cosmic Background Explorer (COBE) spacecraft into low Earth orbit.

Payload

References

References

  1. "Delta 5000".
  2. Wade, Mark. "Delta".
  3. Krebs, Gunter. "Thor Family".
Info: Wikipedia Source

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