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Minotaur I

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Minotaur I
Minotaur I with NFIRE at MARS
Function Small expendable launch system
Manufacturer Northrop Grumman
Country of origin United States
Size
Height 19.21 metres (63.0 ft)
Diameter 1.67 metres (5 ft 6 in)
Mass 36,200 kilograms (79,800 lb)
Stages 4 or 5
Capacity
Payload to LEO
Mass 580 kilograms (1,280 lb)
Payload to SSO
Mass 331 kilograms (730 lb)
Launch history
Status Active
Launch sites Vandenberg SLC-8
MARS LP-0B
Total launches 12
Success(es) 12
First flight 27 January 2000
Last flight 15 June 2021
First stage ? M55A1
Powered by 1 Solid
Maximum thrust 935 kilonewtons (210,000 lb f )
Propellant Solid
Second stage ? SR19
Powered by 1 Solid
Maximum thrust 268 kilonewtons (60,000 lb f )
Propellant Solid
Third stage ? Orion 50XL
Powered by 1 Solid
Maximum thrust 118.2 kilonewtons (26,600 lb f )
Burn time 74 seconds
Propellant Solid
Fourth stage ? Orion 38
Powered by 1 Solid
Maximum thrust 34.8 kilonewtons (7,800 lb f )
Burn time 68 seconds
Propellant Solid

The Minotaur I , or just Minotaur is an American expendable launch system derived from the Minuteman II missile. [1] It is used to launch small satellites for the US Government , and is a member of the Minotaur family of rockets produced by Orbital Sciences Corporation (now Northrop Grumman ). [2]

Vehicle [ edit ]

The Minotaur I is the follow-on to the Orbital Sciences' Taurus (later renamed the "Minotaur-C" [3] ) launch vehicle, combining the original Taurus's booster stage with a second stage from a Minuteman missile . [4]

Minotaur I rockets consist of the M55A1 first stage and SR19 second stage of a decommissioned Minuteman missile. [1] The Orion 50XL and Orion 38 , from the Pegasus rocket, are used as third and fourth stages. A HAPS (Hydrazine Auxiliary Propulsion System) upper stage can also be flown if greater precision is needed, or the rocket needs to be able to manoeuvre to deploy multiple payloads. [5] It can place up to 580 kilograms (1,280 lb) of payload into a 185-kilometer (115 mi) low Earth orbit at 28.5 degrees of inclination . [1]

The Minotaur I is 69 feet tall and 5 feet wide. [6]

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 . [5]

Launch history [ edit ]

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

Minotaur I launch history
Flight Date ( UTC ) Payload Launch pad Trajectory Result
1 January 27, 2000
03:03:06
JAWSat (P98-1) ( FalconSat1 / ASUSat1 / OCSE / OPAL ) Vandenberg SLC-8 LEO Success [7]
2 July 19, 2000
20:09:00
MightySat II.1 (Sindri, P99-1) / MEMS 2A / MEMS 2B Vandenberg SLC-8 LEO Success [8]
3 April 11, 2005
13:35:00
XSS-11
Vandenberg SLC-8
LEO Success [9]
4 September 23, 2005
02:24:00
Streak (STP-R1)
Vandenberg SLC-8
LEO Success [10]
5 April 15, 2006
01:40:00
COSMIC (FORMOSAT-3) Vandenberg SLC-8 LEO Success [11]
6 December 16, 2006
12:00
TacSat-2 / GeneSat-1
MARS LP-0B
LEO Success [12]
7 April 24, 2007
06:48
NFIRE
MARS LP-0B
LEO Success [13]
8 May 19, 2009
23:55
TacSat-3
MARS LP-0B
LEO Success [14]
9 February 6, 2011
12:26
USA-225 (NROL-66)
Vandenberg SLC-8
LEO Success [15]
10 June 30, 2011
03:09
ORS-1
MARS LP-0B
LEO Success [16]
11 November 20, 2013
01:15
ORS-3 , [17] STPSat-3 and 28 CubeSat satellites [18]
MARS LP-0B
LEO Success [19]
12 June 15, 2021
13:35
NROL -111 MARS LP-0B LEO Success [20]


See also [ edit ]

References [ edit ]

  1. ^ a b c "Minotaur I Space Launch Vehicle?Fact Sheet" (PDF) . Orbital Sciences . NASA . 2006. Archived from the original (PDF) on 6 July 2022 . Retrieved 15 June 2021 .
  2. ^ "Minotaur Rocket" . Northrop Grumman . Retrieved 2021-06-07 .
  3. ^ Clark, Stephen (24 February 2014). "Taurus rocket on the market with new name, upgrades" . Spaceflight Now . Retrieved 26 May 2014 .
  4. ^ "Minotaur I Space Launch Vehicle" (PDF) . NASA . 2006. Archived from the original (PDF) on February 25, 2017 . Retrieved March 12, 2023 .
  5. ^ a b "Minotaur I User's Guide - Release 3.0" (PDF) . Orbital Sciences Corporation . Retrieved 1 September 2015 .
  6. ^ "NASA - TacSat-2 Mission Information" . www.nasa.gov . Retrieved 2021-08-03 .
  7. ^ Ray, Justin. "Spaceflight Now - Minotaur Mission Report - Mission Status Center - JAWSAT" . Retrieved 21 April 2013 .
  8. ^ Ray, Justin. "Spaceflight Now - Minotaur Mission Report - Mission Status Center - Mightysat 2.1" . Retrieved 21 April 2013 .
  9. ^ Ray, Justin. "Minotaur rocket launches U.S. military spacecraft" . Spaceflight Now . Retrieved 21 April 2013 .
  10. ^ Ray, Justin. "Rocket launch paints sky with breath-taking scene" . Spaceflight Now . Retrieved 21 April 2013 .
  11. ^ Ray, Justin. "Spaceflight Now - Minotaur Mission Report - Mission Status Center - COSMIC" . Spaceflight Now . Retrieved 21 April 2013 .
  12. ^ Clark, Stephen. "Minotaur rocket makes sunrise ascent from Virginia" . Spaceflight Now . Retrieved 21 April 2013 .
  13. ^ Ray, Justin. "Missile research spacecraft soars into orbit from Virginia" . Spaceflight Now . Retrieved 21 April 2013 .
  14. ^ Clark, Stephen. "Minotaur lofts experimental satellite for U.S. military" . Spaceflight Now . Retrieved 21 April 2013 .
  15. ^ "Orbital Successfully Launches Minotaur I Rocket for U.S. Air Force" . Orbital Sciences Corporation . Retrieved 21 April 2013 .
  16. ^ "Orbital Successfully Launches Minotaur I Rocket Carrying ORS-1 Satellite for the U.S. Air Force" . Orbital Sciences Corporation . Retrieved 21 April 2013 .
  17. ^ "Media Accreditation Open for ORS-3 Mission from Wallops in November" . NASA . 30 October 2013 . Retrieved 30 October 2013 .
  18. ^ "Orbital's Minotaur I successfully lofts multitude of payloads" . NASASpaceFlight.com . 19 November 2013 . Retrieved 20 November 2013 .
  19. ^ "Orbital Successfully Launches Minotaur I Rocket Supporting ORS-3 Mission for the U.S. Air Force" . Wall Street Journal . Retrieved 20 November 2013 .
  20. ^ "Northrop Grumman Successfully Launches Minotaur I Rocket for the National Reconnaissance Office" . Northrop Grumman . 15 June 2021 . Retrieved 15 June 2021 .