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 lbf) |
Propellant | Solid |
Second stage –SR19 | |
Powered by | 1 Solid |
Maximum thrust | 268 kilonewtons (60,000 lbf) |
Propellant | Solid |
Third stage –Orion 50XL | |
Powered by | 1 Solid |
Maximum thrust | 118.2 kilonewtons (26,600 lbf) |
Burn time | 74 seconds |
Propellant | Solid |
Fourth stage –Orion 38 | |
Powered by | 1 Solid |
Maximum thrust | 34.8 kilonewtons (7,800 lbf) |
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]
The Minotaur I is the follow-on to the Orbital Sciences' Taurus (later re-named 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]
There have been twelve launches of the Minotaur I,all successful.
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] |
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