Minotaur (rocket family)

Short description: Family of American rockets

Minotaur on a launch pad at Wallops Flight Facility Minotaur-C in 2017

The Minotaur is a family of United States solid fuel launch vehicles derived from converted Minuteman and Peacekeeper intercontinental ballistic missiles (ICBM). They are built by Northrop Grumman via contract with the Air Force Space and Missile Systems Center's Space Development and Test Directorate (SMC/SD) as part of the Air Force's Rocket Systems Launch Program which converts retired Intercontinental Ballistic Missiles into space and test launch systems for U.S. government agencies.

Three variants of the Minotaur are currently in service. The Minotaur I is an orbital launch system used to launch small satellites into low Earth orbit (LEO). The Minotaur II is a target launch vehicle (TLV), also known as Chimera, used for suborbital flights, often as a target for tracking and anti-ballistic missile tests. The Minotaur IV is a more capable LEO launch system. The Minotaur V is designed to reach higher orbits, including geostationary transfer orbit (GTO) and trans-lunar trajectories. The Minotaur III is a version under development, which will be used for suborbital flights.

The Minotaur I and II are derived from the Minuteman missile, while the Minotaur III, IV and V are derived from the Peacekeeper.

## Contents

* 1 Vehicles
* 1.1 Minotaur-C (Taurus)
* 1.2 Minotaur I
* 1.3 Minotaur II
* 1.4 Minotaur III
* 1.5 Minotaur IV
* 1.6 Minotaur V
* 1.7 Minotaur VI
* 2 Launch statistics
* 2.1 Rocket configurations
* 2.2 Launch sites
* 2.3 Launch outcomes
* 3 Launch history
* 3.1 1994
* 3.2 1998
* 3.3 1999
* 3.4 2000
* 3.5 2001
* 3.6 2002
* 3.7 2004
* 3.8 2005
* 3.9 2006
* 3.10 2007
* 3.11 2008
* 3.12 2009
* 3.13 2010
* 3.14 2011
* 3.15 2013
* 3.16 2017
* 3.17 2020
* 3.18 2021
* 3.19 2022
* 4 Planned launches
* 5 See also
* 6 References
* 7 External links

## Vehicles

### Minotaur-C (Taurus)

The Taurus launch vehicle, later renamed [1] Minotaur-C (for "Minotaur-Commercial"), was the first of the Minotaur vehicle family, and the first ground-launched orbital booster developed by Orbital Sciences Corporation (OSC), derived by adding a solid booster stage to the air-launched Pegasus rocket.

The first flight, sponsored by DARPA, was in 1994. After a series of failures between 2001 and 2011, the launch vehicle was rebranded as Minotaur-C in 2014. Due to laws against selling government equipment, the Minotaur-C is the only available Minotaur launch vehicle for commercial launches.[citation needed]

### Minotaur I

Minotaur I with NFIRE

The original Minotaur launch vehicle, consisting of an M55A1 first stage, SR19 second stage, Orion 50XL third stage, Orion 38 fourth stage, and optional HAPS fifth stage for velocity trim and multiple payload deployment. Payload 580 kg to a 185 km, 28.5° orbit from Cape Canaveral; or 310 kg to a 740 km Sun-synchronous orbit (SSO) from Vandenberg.[2]

### Minotaur II

A suborbital target vehicle, essentially consisting of a Minuteman II with Orbital guidance and control systems. Consists of M55A1 first stage, SR19 second stage, and M57 third stage. Payload 460 kg on 6700 km suborbital trajectory.[2]

### Minotaur III

Minotaur II, Vandenberg

A suborbital target vehicle, consisting of an SR118 first stage, SR119 second stage, SR120 third stage, and Super HAPS fourth stage. Payload 3060 kg on a 6700 km suborbital trajectory.[2]

### Minotaur IV

Minotaur IV, Vandenberg Space Force Base.

The Minotaur IV combines U.S. government-furnished solid rocket motors from decommissioned Peacekeeper ICBMs with technologies from other Orbital-built launch vehicles, including the Minotaur I, Pegasus, and Taurus. The Minotaur IV launch vehicle consists of an SR118 first stage, SR119 second stage, SR120 third stage, and Orion 38 fourth stage. Payload 1735 kg to a 185 km, 28.5° orbit from Cape Canaveral.

The first Minotaur IV was launched 22 April 2010 from Vandenberg Air Force Base in California .[3] This vehicle is also being developed to accommodate the Conventional Prompt Global Strike (CPGS) mission for the Air Force.

### Minotaur V

Minotaur V carrying LADEE

The Minotaur V is a five-stage version based on the Minotaur IV+. It has an additional upper stage for small geostationary transfer orbit (GTO), lunar, and interplanetary missions.

NASA's Lunar Atmosphere and Dust Environment Explorer (LADEE) mission was launched on the first Minotaur V, from the Wallops Island, Virginia launch site at 03:27 UTC on 7 September 2013. The Minotaur launched the LADEE spacecraft into a highly elliptic orbit where it can phase and time its trajectory burn to the moon.[4]

### Minotaur VI

A Minotaur VI five-stage version has also been conceptualized. It is also based on the Minotaur IV+, adding a second SR-118 first stage.[5]

## Launch statistics

### Rocket configurations

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### Launch sites

Script error: No such module "Chart".

### Launch outcomes

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## Launch history

### 1994

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
1  | March 13, 1994
22:32  | Taurus/Minotaur-C (ARPA Taurus)  | Vandenberg Air Force Base , SLC-576E  | STEP Mission 0 and DARPASAT  |  |  | United States Air Force /DARPA[6][7] | Success

### 1998

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
2  | February 10, 1998
13:20  | Taurus/Minotaur-C (Commercial Taurus configuration)  | VAFB SLC-576E  | GFO and Orbcomm (satellites 11,12)  |  |  |  | Success
3  | October 3, 1998
10:04  | Taurus/Minotaur-C (Air Force Taurus Configuration)  | VAFB SLC-576E  | Space Technology Experiment (STEX)  |  |  | NRO  | Success

### 1999

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
4  | December 21, 1999
07:13  | Taurus/Minotaur-C (Model 2110)  | VAFB SLC-576E  | KOMPSAT and ACRIMSAT |  |  |  | Success

### 2000

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
1  | January 27, 2000
03:03:06  | Minotaur I  | Vandenberg Air Force Base SLC-8  | JAWSat (P98-1) (FalconSat1 / ASUSat1 / OCSE / OPAL)  |  | LEO |  | Success
5  | March 12, 2000
09:29  | Taurus/Minotaur-C (Air Force Taurus Configuration)  | VAFB SLC-576E  | Multispectral Thermal Imager (MTI)  |  |  |  | Success
1  | May 28, 2000
20:00  | Minotaur II  | Vandenberg LF-06  | OSP-TLV Missile Defense Technology Demonstrator  |  | Suborbital |  | Success
2  | July 19, 2000
20:09:00  | Minotaur I  | Vandenberg SLC-8  | MightySat II.1 (Sindri, P99-1) / MEMS 2A / MEMS 2B  |  | LEO |  | Success

### 2001

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
6  | September 21, 2001
18:49  | Taurus/Minotaur-C (Model 2110)  | VAFB SLC-576E  | Orbview-4/QuikTOMS |  |  |  | Failure
2  | December 4, 2001
04:59  | Minotaur II  | Vandenberg LF-06  | TLV-1 IFT-7 GMDS target mission  |  | Suborbital |  | Success

### 2002

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
3  | March 16, 2002
02:11  | Minotaur II  | Vandenberg LF-06  | TLV-2 IFT-8 GMDS target mission  |  | Suborbital |  | Success
4  | October 15, 2002
02:01  | Minotaur II  | Vandenberg LF-06  | TLV-3 GMDS target mission  |  | Suborbital |  | Success
5  | December 11, 2002
08:26  | Minotaur II  | Vandenberg LF-06  | TLV-4 GMDS target mission  |  | Suborbital |  | Success

### 2004

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
7  | May 20, 2004
17:47  | Taurus/Minotaur-C (Model 3210)  | VAFB SLC-576E  | ROCSAT-2  |  |  |  | Success

### 2005

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
3  | April 11, 2005
13:35:00  | Minotaur I  | Vandenberg SLC-8  | XSS-11  |  | LEO |  | Success
4  | September 22, 2005
19:24:00  | Minotaur I  | Vandenberg SLC-8  | Streak (STP-R1)  |  | LEO |  | Success

### 2006

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
5  | April 15, 2006
01:40:00  | Minotaur I  | Vandenberg SLC-8  | COSMIC (FORMOSAT-3)  |  | LEO |  | Success
6  | December 16, 2006
12:00  | Minotaur I  | MARS LP-0B  | TacSat-2 / GeneSat-1 |  | LEO |  | Success

### 2007

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
6  | March 21, 2007
04:27  | Minotaur II  | Vandenberg LF-06  | TLV-5 FTX-02 SBR target mission  |  | Suborbital |  | Success
7  | April 24, 2007
06:48  | Minotaur I  | MARS LP-0B  | NFIRE |  | LEO |  | Success
7  | August 23, 2007
08:30  | Minotaur II+  | Vandenberg LF-06  | TLV-7 Mission 2a sensor target for NFIRE satellite  |  | Suborbital |  | Success

### 2008

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
8  | September 24, 2008
06:57  | Minotaur II+  | Vandenberg LF-06  | TLV-8 Mission 2b sensor target for NFIRE satellite  |  | Suborbital |  | Success

### 2009

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
8  | February 24, 2009
09:55  | Taurus/Minotaur-C (Model 3110)  | VAFB SLC-576E  | Orbiting Carbon Observatory[8] |  |  |  | Failure
8  | May 19, 2009
23:55  | Minotaur I  | MARS LP-0B  | TacSat-3 / PharmaSat / AeroCube 3 / HawkSat I / CP6 |  | LEO |  | Success

### 2010

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
1  | April 22, 2010
23:00  | Minotaur IV Lite  | Vandenberg SLC-8  | HTV-2a hypersonic research spacecraft  |  | Suborbital |  | Success
2  | September 26, 2010
04:41  | Minotaur IV  | Vandenberg SLC-8  | SBSS  |  | SSO |  | Success
3  | November 20, 2010
01:25  | Minotaur IV HAPS  | Kodiak LP-1  | STP-S26 (FASTRAC-A / FASTRAC-B / FalconSat-5 / FASTSAT / O/OREOS / RAX)  |  | LEO |  | Success

### 2011

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
9  | February 6, 2011
12:26  | Minotaur I  | Vandenberg SLC-8  | NROL-66  |  | LEO |  | Success
9  | March 4, 2011
10:09  | Taurus/Minotaur-C (Model 3110)  | VAFB SLC-576E  | Glory, KySat-1, Hermes, and Explorer-1 [PRIME] |  |  |  | Failure[9]
10  | June 30, 2011
03:09  | Minotaur I  | MARS LP-0B  | ORS-1  |  | LEO |  | Success
4  | August 11, 2011
14:45  | Minotaur IV Lite  | Vandenberg Air Force Base  | Falcon Hypersonic Technology Vehicle 2 (HTV-2b)  |  | Suborbital |  | Success
5  | September 27, 2011
15:49  | Minotaur IV+  | Kodiak LP-1  | TacSat-4  |  | MEO |  | Success

### 2013

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
1  | September 7, 2013
03:27  | Minotaur V  | MARS LP-0B  | LADEE |  | HEO |  | Success
11  | November 20, 2013
01:15  | Minotaur I  | MARS LP-0B  | ORS-3 (STPSat-3 along with 28 additional cubesats)  |  | LEO |  | Success[10][11]

### 2017

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
6  | August 26, 2017
06:04  | Minotaur IV  | Cape Canaveral Air Force Station , SLC-46  | ORS-5  |  | LEO |  | Success
10  | October 31, 2017
21:37  | Minotaur-C (Model 3210)  | VAFB SLC-576E  | SkySat × 6, Flock-3m × 4  |  |  |  | Success

### 2020

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
7  | July 15, 2020
13:46  | Minotaur IV  | MARS, LP-0B  | NROL-129 (USA 305 to USA 308)[12] |  | LEO | NRO  | Success

### 2021

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
12  | June 15, 2021
13:35[13] | Minotaur I  | MARS, LP-0B  | NROL-111 (USA 316 to USA 318)[14] |  | LEO | NRO  | Success

### 2022

Flight №  | Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Payload mass  | Orbit  | Customer  | Launch
outcome
9  | July 7, 2022
06:01[15] | Minotaur II+  | VSFB, TP-01  | Mk21A reentry vehicle[16] |  | Suborbital | AFNWC  | Failure

## Planned launches

Date / time (UTC)  | Rocket,
Configuration  | Launch site  | Payload  | Orbit  | Customer

|
|
|
|
|

2023[17][18] | Minotaur IV  | VSFB, SLC-8  | NROL-174  | LEO | NRO
2023[17] | TBD  | VSFB  |  |  | U.S. Space Force
September 2024  | Minotaur IV | TBD  | TBD  | LEO | NASA

## See also

* Dnepr, a converted Soviet ICBM often used for commercial satellite launches
* Minotaur-C, the vehicle formerly known as Taurus
* Modified Minotaur IV, Ascent Abort-2 (AA-2), was a suborbital flight to test the Launch Abort System (LAS) of NASA's Orion spacecraft. The suborbital flight used a modified Minotaur IV, launched July 2, 2019, at 11:00 UTC from CCAFS SLC-46. The suborbital flight was a success. Reference: Wikipedia article Ascent Abort-2.

## References

1. ↑ Stephen Clark, "Taurus rocket on the market with new name, upgrades", Spaceflight Now 24 February 2014
2. ↑ 2.0 2.1 2.2 "Minotaur". Encyclopedia Astronautix. http://www.astronautix.com/lvs/minotaur.htm.
3. ↑ "Minotaur IV". Orbital Sciences Corporation. http://www.orbital.com/SpaceLaunch/Minotaur/IV/.
4. ↑ Culler, Jessica (16 June 2015). "LADEE - Lunar Atmosphere Dust and Environment Explorer". NASA. http://www.nasa.gov/mission_pages/ladee/main/index.html#.UhaLbJLryXs. This article incorporates text from this source, which is in the public domain.
5. ↑ "Orbital ATK". Orbital Sciences Corporation. http://www.orbital.com/NewsInfo/Publications/Minotaur6_Fact.pdf.
6. ↑ "DARPASAT". https://space.skyrocket.de/doc_sdat/darpasat.htm.
7. ↑ "Encyclopedia Astronautica: TAOS". Encyclopedia Astronautica. http://www.astronautix.com/s/step0taosp90-5.html.
8. ↑ "OCO". Orbital Sciences Corporation. http://www.orbital.com/SatellitesSpace/ScienceTechnology/OCO/.
9. ↑ "Taurus rocket nose shroud dooms another NASA satellite". Spaceflight Now, March 2011. http://www.spaceflightnow.com/taurus/glory/110304gloryfail/.
10. ↑ Powell, Rebecca (16 April 2015). "Air Force Minotaur Rocket Launching from Virginia November 19". http://www.nasa.gov/content/air-force-minotaur-rocket-launching-from-virginia-november-19/#.UqDMg_lJPDE.
11. ↑ "ORS-3 and STPSat-3 Successfully Launched". http://www.losangeles.af.mil/News/Article-Display/Article/734800/ors-3-and-stpsat-3-successfully-launched/.
12. ↑ Krebs, Gunter (25 August 2021). "USA 305, ..., 308 (NROL 129 PL1, ..., 4)". Gunter's Space Page. https://space.skyrocket.de/doc_sdat/usa-305.htm.
13. ↑ "Northrop Grumman Successfully Launches Minotaur I Rocket for the National Reconnaissance Office". Northrop Grumman. 15 June 2021. https://news.northropgrumman.com/news/releases/northrop-grumman-successfully-launches-minotaur-i-rocket-for-the-national-reconnaissance-office.
14. ↑ Krebs, Gunter (24 June 2021). "USA 316, 317, 318 (NROL 111)". Gunter's Space Page. https://space.skyrocket.de/doc_sdat/usa-316.htm.
15. ↑ Scully, Janene (7 July 2022). "Missile Test Ends in Explosion Seconds After Launch from Vandenberg SFB". Noozhawk. https://www.noozhawk.com/article/missile_test_ends_in_explosion_seconds_after_launch_from_vandenberg_sfb.
16. ↑ Martinez-Pogue, Jade (6 July 2022). "Test rocket launch scheduled from Vandenberg Space Force Base Thursday morning". KEYT-TV. https://keyt.com/news/santa-maria-north-county/2022/07/06/test-rocket-launch-scheduled-from-vandenberg-space-force-base-thursday-morning/.
17. ↑ 17.0 17.1 Navin, Joseph (1 September 2021). "Northrop Grumman discusses Antares NG-16's eventful countdown, talks future missions". NASASpaceFlight. https://www.nasaspaceflight.com/2021/09/ng-16-update/. ""We're basically on contract for three Minotaur launches. One is a Minotaur IV, which looks like it's going to be launched from Vandenberg Space Force Base in 2023, and that's for the Space Force," said Eberly. In total, there will be one Minotaur launch in 2022 and two launches in 2023. All three of these missions will launch from Vandenberg Space Force Base in California and will be flown for the U.S. Space Force."
18. ↑ Clark, Stephen (15 June 2021). "NRO satellites launched by Minotaur rocket with surplus missile parts". Spaceflight Now. https://spaceflightnow.com/2021/06/15/three-nro-satellites-launched-by-minotaur-rocket-with-surplus-missile-parts/. "[T]he Space Force and the NRO have purchased at least one more Minotaur flight to deliver another classified payload to orbit. That mission, known as NROL-174, will use a Minotaur 4 rocket, the larger Minotaur variant. It is scheduled for launch in 2023, Eberly said."

## External links

* Minotaur I Rocket page
* Minotaur IV Rocket page
* NASA Astronomy Picture of the Day: Image of the September 2005 launch (28 September 2005)
* Encyclopedia Astronautix Entry for Minotaur

* v
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Rocket families

Carrier rockets|

| China|

* Long March
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|

France / ESA|

* Ariane
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India|

* PSLV
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Japan|

* Epsilon
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United States|

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Other nations|

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Sounding rockets|

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Missiles|

* Aggregat
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* Some families include both missiles and carrier rockets; they are listed in both groups.

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Orbital launch systems

* List of orbital launch systems
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Current|

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In development|

* Angara 1.2
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Classes|

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* Symbol † indicates projects terminated before a successful orbital launch

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Orbital launch systems developed in the United States

Active|

* Antares 230+
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* I
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In development|

* Firefly Alpha
* Beta
* LauncherOne
* New Glenn
* OmegA
* SLS
* Starship
* Vector-R
* Vector-H
* Vulcan

Retired|

* Antares 110/120/130/230
* Athena
* I
* II
* Atlas
* B
* D
* E/F
* G
* H
* I
* II
* III
* LV-3B
* SLV-3
* Able
* Agena
* Centaur
* Conestoga
* Delta
* A
* B
* C
* D
* E
* G
* J
* L
* M
* N
* 0100
* 1000
* 2000
* 3000
* 4000
* 5000
* II
* III
* IV
* Falcon 1
* Falcon 9
* v1.0
* v1.1
* v1.2 "Full Thrust"
* H-I*
* Juno I
* Juno II
* N-I*
* N-II*
* Pilot
* Saturn
* I
* IB
* V
* Scout
* Space Shuttle
* SPARK
* Sparta
* Thor
* Able
* Ablestar
* Agena
* Burner
* Delta
* DSV-2U
* Thorad-Agena
* Titan
* II GLV
* IIIA
* IIIB
* IIIC
* IIID
* IIIE
* 34D
* 23G
* CT-3
* IV
* Vanguard

* * - Japanese projects using US rockets or stages

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Original source: https://en.wikipedia.org/wiki/Minotaur (rocket family). Read more

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