Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Delta 5000

From Wikipedia, the free encyclopedia
Series of American expendable launch systems
Delta 5000 series
Launch of the Delta 5920 withCOBE
FunctionExpendable launch system
Country of originUnited States
Cost per launchUS$34.22 million in 1985[1] (US$79.99 million in 2018)
Size
Height34 m (112 ft)
Diameter2.44 m (8 ft 0 in)
Mass201,580 kg (444,410 lb)
Stages2
Capacity
Payload toLEO
Mass3,848 kg (8,483 lb)
Payload toGTO
Mass1,405 kg (3,097 lb)
Associated rockets
FamilyDelta
ComparableDelta 4000,Delta II
Launch history
StatusRetired
Launch sitesVandenbergSLC-2W
Total launches1
Success(es)1
UTC date of spacecraft launch18 November 1989
Boosters –Castor 4A
No. boosters9
Height9.12 m (29.9 ft)
Diameter1.02 m (3 ft 4 in)
Empty mass1,529 kg (3,371 lb)
Gross mass11,743 kg (25,889 lb)
Powered bySolid
Maximum thrust478.3 kN (107,500 lbf)
Specific impulse
    • Sea level: 237 seconds
    • Vacuum: 266 seconds
Burn time56 s
First stage – Thor/Delta ELT
Height22.37 m (73.4 ft)
Diameter2.44 m (8 ft 0 in)
Empty mass4,360 kg (9,610 lb)
Gross mass84,368 kg (186,000 lb)
Powered by1RS-27
Maximum thrust1,030.2 kN (231,600 lbf)
Specific impulse
    • Sea level: 262 seconds
    • Vacuum: 296 seconds
Burn time223 s
PropellantLOX /RP-1
Second stage –Delta K
Height5.89 m (19.3 ft)
Diameter2.44 m (8 ft 0 in)
Empty mass950 kg (2,090 lb)
Gross mass6,954 kg (15,331 lb)
Powered by1AJ10-118K
Maximum thrust43.6 kN (9,800 lbf)
Specific impulse319 s
Burn time431 s
PropellantN2O4 /Aerozine 50

TheDelta 5000 series was an Americanexpendable launch system which was used to conduct anorbital launch in 1989. It was a member of theDelta family of rockets. Although several variants were put forward, only the Delta 5920 was launched. The designation used afour 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 theDelta II 6000-series, which was just entering service.

The first stage was theRS-27 poweredExtended Long Tank Thor, flown on several earlier Delta rockets. NineCastor-4Asolid rocket boosters were attached to increase thrust at lift-off, replacing the less powerfulCastor-4 boosters used on the 3000 series. TheDelta-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, fromSpace Launch Complex 2W at theVandenberg Air Force Base. Launch occurred at 14:34 on 18 November 1989. It was successful, and placed theCosmic Background Explorer (COBE) spacecraft intolow Earth orbit.[2][3]

Payload

[edit]
This section is an excerpt fromCosmic Background Explorer.[edit]
Artist's concept of the COBE spacecraft

TheCosmic Background Explorer (COBE/ˈkbi/KOH-bee), also referred to as Explorer 66, was aNASA satellite dedicated tocosmology, which operated from 1989 to 1993. Its goals were to investigate thecosmic microwave background radiation (CMB or CMBR) of theuniverse and provide measurements that would help shape the understanding of thecosmos.

COBE's measurements provided two key pieces of evidence that supported theBig Bang theory of the universe: that the CMB has a near-perfectblack-bodyspectrum, and that it has very faintanisotropies. Two of COBE's principal investigators,George F. Smoot III andJohn C. Mather, received theNobel Prize in Physics in 2006 for their work on the project. According to the Nobel Prize committee, "the COBE project can also be regarded as the starting point forcosmology as a precision science".[4]

COBE was the second cosmic microwave background satellite, followingRELIKT-1, and was followed by two more advanced spacecraft: theWilkinson Microwave Anisotropy Probe (WMAP) operated from 2001 to 2010 and thePlanck spacecraft from 2009 to 2013.

References

[edit]
  1. ^"Delta 5000". Archived fromthe original on September 16, 2016.
  2. ^Wade, Mark."Delta". Archived fromthe original on 2008-07-24.
  3. ^Krebs, Gunter."Thor Family".Gunter's Space Page.Archived from the original on 2007-08-06. Retrieved2021-12-21.
  4. ^"The Nobel Prize in Physics 2006". The Royal Swedish Academy of Sciences. 2006-10-03. Retrieved2011-08-23.
Current
In development
Retired
Classes
  • This template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
  • Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
Orbitallaunch systems developed in the United States
Active
In development
Retired
  • * - Japanese projects using US rockets or stages
  • ** - uses Russian engines
  • - never succeeded
  • †† - no new orders accepted and production stopped
  • ††† - used Ukrainian first stage
Thor and Delta rockets
Rockets
Thor
Delta
Alphabetical
Numerical
Modern
Export
Launch sites
Canaveral
Johnston
Tanegashima
Vandenberg
Bases
Components
Boosters
First stages
Upper Stages
Delta
Other
Engines
Manufacturers
Rocket
Engines
Launches
Retrieved from "https://en.wikipedia.org/w/index.php?title=Delta_5000&oldid=1297218979"
Category:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp