Minotaur I

Space launch vehicle


title: "Minotaur I" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["minotaur-(rocket-family)"] description: "Space launch vehicle" topic_path: "general/minotaur-rocket-family" source: "https://en.wikipedia.org/wiki/Minotaur_I" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::summary Space launch vehicle ::

::data[format=table title="Infobox Rocket"]

FieldValue
nameMinotaur I
imageNFIRE1.jpg
captionMinotaur I with NFIRE at MARS
functionSmall expendable launch system
manufacturerNorthrop Grumman
country-originUnited States
height19.21 m
diameter1.67 m
mass36200 kg
stages4 or 5
locationLEO
kilos580 kg }}
locationSSO
kilos331 kg }}
statusActive
sitesVandenberg SLC-8
MARS LP-0B
first27 January 2000
last18 June 2024
launches13
success13
typestage
stagenoFirst
nameM55A1
engines1 Solid
thrust935 kN
fuelSolid
typestage
stagenoSecond
nameSR19
engines1 Solid
thrust268 kN
fuelSolid
typestage
stagenoThird
nameOrion 50XL
engines1 Solid
thrust118.2 kN
burntime74 seconds
fuelSolid
typestage
stagenoFourth
nameOrion 38
engines1 Solid
thrust34.8 kN
burntime68 seconds
fuelSolid
::

|name = Minotaur I |image = NFIRE1.jpg |caption = Minotaur I with NFIRE at MARS |function = Small expendable launch system |manufacturer = Northrop Grumman |country-origin = United States |height = 19.21 m |diameter = 1.67 m |mass = 36200 kg |stages = 4 or 5 |capacities = |location = LEO |kilos = 580 kg }} |location = SSO |kilos = 331 kg }} |status = Active |sites = Vandenberg SLC-8 MARS LP-0B |first= 27 January 2000 |last= 18 June 2024 |launches = 13 |success = 13 |stagedata = |type = stage |stageno = First |name = M55A1 |engines = 1 Solid |thrust = 935 kN |burntime = |fuel = Solid |type = stage |stageno = Second |name = SR19 |engines = 1 Solid |thrust = 268 kN |burntime = |fuel = Solid |type = stage |stageno = Third |name = Orion 50XL |engines = 1 Solid |thrust = 118.2 kN |burntime = 74 seconds |fuel = Solid |type = stage |stageno = Fourth |name = Orion 38 |engines = 1 Solid |thrust = 34.8 kN |burntime = 68 seconds |fuel = Solid The Minotaur I, or just Minotaur is an American expendable launch system derived from the Minuteman II missile.

Vehicle

The Minotaur I is the follow-on to the Orbital Sciences' Taurus (later renamed the "Minotaur-C") launch vehicle, combining the original Taurus's booster stage with a second stage from a Minuteman missile.

Minotaur I rockets consist of the M55A1 first stage and SR19 second stage of a decommissioned Minuteman missile. It can place up to 580 kg of payload into a 185 km low Earth orbit at 28.5 degrees of inclination.

The Minotaur I is 69 feet tall and 5 feet wide.

Initially Minotaur I launches are conducted from Space Launch Complex 8 at the Vandenberg Air Force Base. Starting with the launch of TacSat-2 in December 2006, launches have also been conducted from Pad 0B at the Mid-Atlantic Regional Spaceport on Wallops Island.

Launch history

There have been thirteen launches of the Minotaur I, all successful.

::data[format=table title="Minotaur I launch history"]

FlightDate (UTC)PayloadLaunch padTrajectoryResult
1January 27, 2000
03:03:06JAWSat (P98-1) (FalconSat1 / ASUSat1 / OCSE / OPAL)Vandenberg SLC-8LEO
2July 19, 2000
20:09:00MightySat II.1 (Sindri, P99-1) / MEMS 2A / MEMS 2BVandenberg SLC-8LEO
3April 11, 2005
13:35:00XSS-11[[File:Minotaur rocket launch.jpgframeless150x150px]]
Vandenberg SLC-8LEO
4September 23, 2005
02:24:00Streak (STP-R1)[[File:Minotaur 1 with Streak (23 Sep. 2005).jpgframeless150x150px]]
Vandenberg SLC-8LEO
5April 15, 2006
01:40:00COSMIC (FORMOSAT-3)Vandenberg SLC-8LEO
6December 16, 2006
12:00TacSat-2 / GeneSat-1[[File:Minotaur awaiting launch.jpgframeless150x150px]]
MARS LP-0BLEO
7April 24, 2007
06:48NFIRE[[File:NFIRE1.jpgframeless150x150px]]
MARS LP-0BLEO
8May 19, 2009
23:55TacSat-3[[File:TacSat3 launch 090518-F-9999B-001 (cropped).jpgframeless150x150px]]
MARS LP-0BLEO
9February 6, 2011
12:26USA-225 (NROL-66)[[File:Minotaur-1 NROL-66.jpgframeless150x150px]]
Vandenberg SLC-8LEO
10June 30, 2011
03:09ORS-1[[File:Minotaur I with ORS-1 on MARS pad 0B (110622-F-PF707-001).jpgframeless150x150px]]
MARS LP-0BLEO
11November 20, 2013
01:15ORS-3,
12June 15, 2021
13:35NROL-111MARS LP-0BLEO
13June 18, 2024
07:01Mk21A reentry vehicle test[[File:MINOTAUR I ROCKET LAUNCHES FROM VSFB (8505466).jpgframeless100x100px]]
Vandenberg TP-01Suborbital
::

References

References

  1. "Minotaur Rocket".
  2. Clark, Stephen. (24 February 2014). "Taurus rocket on the market with new name, upgrades". Spaceflight Now.
  3. (2006). "Minotaur I Space Launch Vehicle".
  4. (2006). "Minotaur I Space Launch Vehicle—Fact Sheet". [[NASA]].
  5. "NASA - TacSat-2 Mission Information".
  6. Ray, Justin. "Spaceflight Now - Minotaur Mission Report - Mission Status Center - JAWSAT".
  7. Ray, Justin. "Spaceflight Now - Minotaur Mission Report - Mission Status Center - Mightysat 2.1".
  8. Ray, Justin. "Minotaur rocket launches U.S. military spacecraft". Spaceflight Now.
  9. Ray, Justin. "Rocket launch paints sky with breath-taking scene". Spaceflight Now.
  10. Ray, Justin. "Spaceflight Now - Minotaur Mission Report - Mission Status Center - COSMIC". Spaceflight Now.
  11. Clark, Stephen. "Minotaur rocket makes sunrise ascent from Virginia". Spaceflight Now.
  12. Ray, Justin. "Missile research spacecraft soars into orbit from Virginia". Spaceflight Now.
  13. Clark, Stephen. "Minotaur lofts experimental satellite for U.S. military". Spaceflight Now.
  14. "Orbital Successfully Launches Minotaur I Rocket for U.S. Air Force". [[Orbital Sciences Corporation]].
  15. "Orbital Successfully Launches Minotaur I Rocket Carrying ORS-1 Satellite for the U.S. Air Force". [[Orbital Sciences Corporation]].
  16. (19 November 2013). "Orbital's Minotaur I successfully lofts multitude of payloads". [[NASASpaceFlight.com]].
  17. "Orbital Successfully Launches Minotaur I Rocket Supporting ORS-3 Mission for the U.S. Air Force". [[Wall Street Journal]].
  18. (15 June 2021). "Northrop Grumman Successfully Launches Minotaur I Rocket for the National Reconnaissance Office". [[Northrop Grumman]].
  19. Hadley, Greg. (2024-06-18). "Air Force, Lockheed Test New Reentry Vehicle for Sentinel ICBM".

::callout[type=info title="Wikipedia Source"] This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page. ::

minotaur-(rocket-family)