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{{short description|None}} | |||
{{Infobox rocket | |||
|image = Delta III.svg | |||
⚫ | ''']''' was an ] made by ]. The first Delta III launch was on August 26, 1998.<ref name=wired>{{Cite magazine|url=https://www.wired.com/1998/08/delta-iii-takes-a-dip/|title=Delta III Takes a Dip|magazine=WIRED|access-date=2018-10-24|language=en-US}}</ref> Of its three flights, the first two were failures, and the third, though declared successful, reached the low end of its targeted orbit range and carried only a dummy (inert) payload. The Delta III could deliver up to 8,400 pounds (3,800 kilograms) to ], twice the payload of its predecessor, the ].<ref name=":0">{{Cite web|url = http://www.boeing.com/defense-space/space/delta/delta3/delta3.htm|title = Delta III Launch Vehicle|date = 2001|archive-url = https://web.archive.org/web/20011114221110/http://www.boeing.com/defense-space/space/delta/delta3/delta3.htm|archive-date = November 14, 2001}}</ref> Under the four-digit designation system from earlier ] rockets, the Delta III is classified as the Delta 8930. | ||
|upright = 0.4 | |||
|caption =A Delta III rocket | |||
|name = Delta III | |||
|function = Orbital ] | |||
|manufacturer = ]<small><br>(design, manufacturing and assembly)</small><br> | |||
]<br><small>(extended kerosene tank and ]-based upper stage manufacturing)</small> | |||
|country-origin = United States | |||
⚫ | | |
||
⚫ | | |
||
⚫ | | |
||
|stages = 2 | |||
|capacities = <!--insert one of the following templates for each payload:--> | |||
{{Infobox rocket/payload | |||
|location = ] | |||
|kilos = {{cvt|8,290|kg}}<ref name=":0"/> | |||
}} | |||
{{Infobox rocket/payload | |||
|location = ] | |||
|kilos = {{cvt|3,810|kg}}<ref name=":0"/> | |||
}} | |||
|status = Retired | |||
|family=] | |||
|sites = ], ] | |||
|launches = 3 | |||
|success = 0 | |||
|partial = 1 | |||
|fail = 2 | |||
|first=August 26, 1998 | |||
|last=August 23, 2000 | |||
|stagedata = | |||
{{Infobox rocket/stage | |||
|type = booster | |||
|number = 9 ] | |||
|solid = yes | |||
|thrust = {{cvt|628.3|kN}} | |||
|SI = {{convert|273|isp}} | |||
|burntime = 75 seconds | |||
|fuel = ] mix, similar to ] | |||
}} | |||
{{Infobox rocket/stage | |||
|type = stage | |||
|diff = <!--variant of rocket this is used on, optional--> | |||
|stageno = First | |||
|name = <!--name of the stage/booster, optional--> | |||
|engines = 1 ] ] | |||
|thrust = {{cvt|1085.79|kN}} | |||
|SI = {{convert|254|isp}} | |||
|burntime = 260 seconds<ref name=d3ppg>{{cite web|url=http://www.boeing.com/defense-space/space/delta/docs/DELTA_III_PPG_2000.PDF|title=Delta III Payload Planner's Guide|archive-url=https://web.archive.org/web/20011119102909/http://www.boeing.com/defense-space/space/delta/docs/DELTA_III_PPG_2000.PDF|archive-date=19 November 2001}}</ref> | |||
|fuel = ]/] | |||
}} | |||
{{Infobox rocket/stage | |||
|type = stage | |||
|diff = <!--variant of rocket this is used on, optional--> | |||
|stageno = Second | |||
|name = <!--name of the stage/booster, optional--> | |||
|engines = 1 ] ] | |||
|thrust = {{cvt|110.03|kN}} | |||
|SI = {{convert|462|isp}}<ref name=slrd3>{{cite web|title=Delta III Data Sheet|url=http://www.spacelaunchreport.com/delta3.html|website=Space Launch Report|access-date=26 July 2014}}</ref> | |||
|burntime = 700 seconds<ref name=d3ppg/> | |||
|fuel = ]/] | |||
}} | |||
{{Infobox rocket/stage | |||
|type = stage | |||
|diff = Optional | |||
|stageno = Third | |||
|engines = 1 ] ] | |||
|solid = yes | |||
|thrust = {{cvt|66.723|kN}} | |||
|SI = {{convert|286|isp}} | |||
|burntime = 87 seconds | |||
|fuel = ] | |||
}} | |||
}} | |||
⚫ | '''Delta III''' was an ] made by ]. The first Delta III launch was on August 26, 1998.<ref name=wired>{{Cite |
||
== Launch outcome statistics == | == Launch outcome statistics == | ||
{{ #invoke:Chart | bar chart | {{ #invoke:Chart | bar chart | ||
| float = center | | float = center | ||
| width = 500 | | width = 500 | ||
| height = |
| height = 200 | ||
| stack = 1 | | stack = 1 | ||
| group 1 = 1:1:0 | | group 1 = 1:1:0 | ||
| group 2 = 0:0:1 | | group 2 = 0:0:1 | ||
| colors = |
| colors = FireBrick : Orange | ||
| group names = |
| group names = Failure : Partial Failure | ||
| x legends = ] : ] : ] | | x legends = ] : ] : ] | ||
| y tick marks = 1 | | y tick marks = 1 | ||
}} | }} | ||
== Launch |
== Launch history == | ||
{| class="wikitable sortable mw-collapsible plainrowheaders" style="width: 72%;" | |||
{| class="wikitable sortable" | |||
|+ | |+ | ||
|- | |- | ||
Line 103: | Line 31: | ||
! scope="col" | Launch <br /> outcome | ! scope="col" | Launch <br /> outcome | ||
|- | |- | ||
! rowspan="2" scope="row" style="text-align:center;" | |
! rowspan="2" scope="row" style="text-align:center;" |1 | ||
| August 27, 1998<br />01:17 | | August 27, 1998<br />01:17 | ||
| |
| Delta III 8930 | ||
| ] | | ] | ||
| Galaxy 10 | | Galaxy 10 | ||
⚫ | | {{cvt|700|kg}} | ||
| 1,543 pounds (700 kilograms) | |||
| ] | | ] | ||
| ] / ] | | ] / ] | ||
| {{Failure}} | | {{Failure}} | ||
|- | |- | ||
| colspan="8" |Maiden flight of |
| colspan="8" |Maiden flight of Delta III. Destroyed by range safety after control problems and depletion of hydraulic fluid. ]. | ||
|- | |- | ||
! rowspan="2" | |
! rowspan="2" |2 | ||
|May 5, 1999<br />01:00 | |May 5, 1999<br />01:00 | ||
| |
|Delta III 8930 | ||
|] | | ] | ||
|] | | ] | ||
⚫ | | {{cvt|4300|kg}} | ||
|9,480 pounds (4,300 kilograms) | |||
|] | | ] | ||
|] | | ] | ||
| {{Failure}}<ref>{{cite web |url=https://sky-brokers.com/satellite/orion-3-at-139-east-launch-failure/ |title=Orion 3 at 139° East (Launch failure) |access-date=7 September 2022}}</ref> | |||
| {{Failure}} | |||
|- | |- | ||
| colspan="8" |Second stage engine failure. Payload placed |
| colspan="8" |Second stage engine failure. Payload placed in ], declared too low and ] called satellite lost. Communications satellite. | ||
|- | |- | ||
! rowspan=" |
! rowspan="2" |3 | ||
| August 23, 2000<br/>11:05 | | August 23, 2000<br/>11:05 | ||
| |
| Delta III 8930 | ||
| ] | | ] | ||
| DM-F3 | | DM-F3 | ||
⚫ | | {{cvt|4383|kg}} | ||
| 9,663 pounds (4,383 kilograms) | |||
| ] | | ] | ||
| ] | | ] | ||
| {{Partial failure}}<ref name=delta280>{{cite web|url=http://www.spaceflightnow.com/delta/d280/000824loworbit.html|title=Delta 3 rocket falls short but still a success, Boeing says|date=August 24, 2000|publisher=Spaceflight Now}}</ref> | | {{Partial failure}}<ref name=delta280>{{cite web|url=http://www.spaceflightnow.com/delta/d280/000824loworbit.html|title=Delta 3 rocket falls short but still a success, Boeing says|date=August 24, 2000|publisher=Spaceflight Now}}</ref> | ||
|- | |- | ||
| colspan="8" |Reached lower than planned orbit |
| colspan="8" |Reached lower than planned orbit. Final flight of Delta III. Payload was a ]. | ||
|- | |- | ||
|} | |} | ||
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== References == | == References == | ||
{{Reflist}} | {{Reflist}} | ||
{{DEFAULTSORT:Delta 3, list of launches}} | |||
] | |||
] |
Latest revision as of 21:24, 18 July 2024
Delta III was an expendable launch vehicle made by Boeing. The first Delta III launch was on August 26, 1998. Of its three flights, the first two were failures, and the third, though declared successful, reached the low end of its targeted orbit range and carried only a dummy (inert) payload. The Delta III could deliver up to 8,400 pounds (3,800 kilograms) to geostationary transfer orbit, twice the payload of its predecessor, the Delta II. Under the four-digit designation system from earlier Delta rockets, the Delta III is classified as the Delta 8930.
Launch outcome statistics
1 1998 1999 2000- Failure
- Partial Failure
Launch history
Flight Number | Date / time (UTC) | Rocket Configuration |
Launch site | Payload | Payload mass | Orbit | Customer | Launch outcome |
---|---|---|---|---|---|---|---|---|
1 | August 27, 1998 01:17 |
Delta III 8930 | CCAFS SLC-17B | Galaxy 10 | 700 kg (1,500 lb) | GTO | PanAmSat / Intelsat | Failure |
Maiden flight of Delta III. Destroyed by range safety after control problems and depletion of hydraulic fluid. Communications satellite. | ||||||||
2 | May 5, 1999 01:00 |
Delta III 8930 | CCAFS SLC-17B | Orion 3 | 4,300 kg (9,500 lb) | GTO | Loral | Failure |
Second stage engine failure. Payload placed in low Earth orbit, declared too low and Loral called satellite lost. Communications satellite. | ||||||||
3 | August 23, 2000 11:05 |
Delta III 8930 | CCAFS SLC-17B | DM-F3 | 4,383 kg (9,663 lb) | GTO | US Air Force | Partial failure |
Reached lower than planned orbit. Final flight of Delta III. Payload was a DemoSat. |
References
- "Delta III Takes a Dip". WIRED. Retrieved 2018-10-24.
- "Delta III Launch Vehicle". 2001. Archived from the original on November 14, 2001.
- "Orion 3 at 139° East (Launch failure)". Retrieved 7 September 2022.
- "Delta 3 rocket falls short but still a success, Boeing says". Spaceflight Now. August 24, 2000.