Minotaur-C

Minotaur-C (Taurus)

Minotaur-C launching its return-to-flight in 2017
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First stage – Castor 120
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Second stage – Taurus-1
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Third stage – Pegasus-2
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Fourth stage – Pegasus-3
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Minotaur-C (Minotaur Commercial), formerly known as Taurus or Taurus XL, is a four stage solid fueled launch vehicle built in the United States by Orbital Sciences (now Northrop Grumman) and launched from SLC-576E at California's Vandenberg Air Force Base. It is based on the air-launched Pegasus rocket from the same manufacturer, utilizing a "zeroth stage" in place of an airplane. The Minotaur-C is able to carry a maximum payload of around 1458 kg into a low Earth orbit (LEO).

First launched in 1994, it has successfully completed seven out of a total of ten military and commercial missions. Three of four launches between 2001 and 2011 ended in failure, including the 24 February 2009 launch of the Orbiting Carbon Observatory mission and the 4 March 2011 launch of the Glory mission, which resulted in losses totalling US$700 million for NASA (excluding the cost of the rockets themselves). The Taurus launch vehicle was subsequently rebranded in 2014 as Minotaur-C, which incorporates new avionics based on those used by the Minotaur family of rockets. After a six years pause, the rocket successfully returned to flight in 2017 as Minotaur-C.

Stages

The Minotaur-C's first stage, an Orbital ATK Castor 120, is based on a Peacekeeper ICBM first stage. Stages 2 and 3 are Orion-50s (like the Pegasus-1 but without wings or stabilisers), and stage 4 is an Orion 38, derived from the Pegasus-3.

Numbering system

Different configurations are designated using a four-digit code, similar to the numbering system used on Delta rockets. The first digit denotes the type of first stage being used, and whether the second and third stages use a standard or "XL" configuration. The second digit denotes the diameter of the payload fairing. The third digit denotes the type of fourth stage. The fourth digit denotes an optional fifth stage, so far unused.

Number	First digit			Second Digit	Third Digit	Fourth Digit
	First stage	Second stage	Third stage	Fairing diameter	Fourth stage	Fifth stage
0	—Template:Screen reader-only			—Template:Screen reader-only	—Template:Screen reader-only	None
1	TU-903	Orion 50ST	Orion 50T	1.60 m (63 in)	Orion 38	—Template:Screen reader-only
2	Castor-120	Orion 50ST	Orion 50T	2.34 m (92 in)	—Template:Screen reader-only	—Template:Screen reader-only
3	Castor-120	Orion 50SXLT	Orion 50XLT	—Template:Screen reader-only	Star-37FM	Star-37

Launch history

Flight No.	Date/Time (UTC)	Vehicle type	Launch site	Payload	Result
1	13 March 1994 22:32	ARPA Taurus	VAFB, SLC-576E	STEP Mission 0 and DARPASAT	Template:Success
2	10 February 1998 13:20	Commercial Taurus, 92" payload fairing and 63" dual payload attach fitting	VAFB, SLC-576E	GFO and Orbcomm (satellite 11 and 12)	Template:Success
3	3 October 1998 10:04	Air Force Taurus Configuration, 63" fairing, Peacekeeper Stage 0	VAFB, SLC-576E	Space Technology Experiment (STEX) for National Reconnaissance Office (NRO)	Template:Success
4	21 December 1999 07:13	Model 2110, 63" fairing, Castor 120 Stage 0	VAFB, SLC-576E	KOMPSAT and ACRIMSAT	Template:Success
5	12 March 2000 09:29	Air Force Taurus Configuration, 63" fairing, Peacekeeper Stage 0	VAFB, SLC-576E	Multispectral Thermal Imager (MTI)	Template:Success
6	21 September 2001 18:49	Model 2110, 63" fairing, Castor 120 Stage 0	VAFB, SLC-576E	Orbview-4 / QuikTOMS	Failure
7	20 May 2004 17:47	Model 3210, 92" fairing, Castor 120 Stage 0	VAFB, SLC-576E	ROCSAT-2	Template:Success
8	24 February 2009 09:55	Model 3110, 63" fairing, Castor 120 Stage 0	VAFB, SLC-576E	Orbiting Carbon Observatory	Failure
9	4 March 2011 10:09	Model 3110, 63" fairing, Castor 120 Stage 0	VAFB, SLC-576E	Glory, KySat-1, Hermes, and Explorer-1 [PRIME]	Failure
10	31 October 2017 21:37	Model 3210, 92" fairing, Castor 120 Stage 0	VAFB, SLC-576E	SkySat x 6, Flock-3m x 4	Template:Success

Launch failures

Orbview-4

On 21 September 2001, a Taurus XL rocket failed during launch. When the second stage ignited at T+83 seconds, a nozzle gimbal actuator drive shaft seized for approximately 5 seconds causing loss of control. The vehicle recovered and continued to fly the mission profile, but failed to reach a stable orbit and reentered near Madagascar.

Orbiting Carbon Observatory

On 24 February 2009, a Taurus XL rocket failed during the launch of the US$270 million Orbiting Carbon Observatory spacecraft. Liftoff occurred successfully at 09:55 UTC from Vandenberg Air Force Base, but data received at a later stage of the flight suggested that the fairing failed to separate. The rocket did not reach orbit, owing to the extra weight of the fairing. Launch vehicle and services for OCO are estimated at US$54 million. The replacement satellite, Orbiting Carbon Observatory 2, was launched on 2 July 2014 aboard a Delta II rocket.

Glory

On 4 March 2011, a Taurus XL rocket failed again during the launch of NASA's US$424 million Glory climate change monitoring satellite. In total, the last two failures of the Taurus XL have resulted in payload losses worth $700 million. The reason for the failure was the same as with OCO: the payload fairing failed to separate, although the rocket's manufacturer Orbital Sciences Corporation had spent the last two years trying to fix the problem and had made several design changes to the fairing separation system. Ronald Grabe, manager of Orbital Sciences Corporation, which also built the Glory satellite itself, said the employees of his companies are "pretty devastated" because of the latest failure. The fairing was built by the Vermont Composites company, and the frangible rail pyrotechnic separation system was built by the Ensign-Bickford Company. A NASA MIB panel concluded that the failure was most likely caused by a section of the frangible rail somewhere near the nose cap failing to separate. While a root cause could not be identified, two likely causes were identified: the rubber charge holder in the frangible rail slumping due to launch acceleration and random vibration, or a failure of the frangible rail system due to it operating outside the environment for which it was tested.

A continued investigation eventually revealed that sub-standard parts provided by Sapa Profiles, Inc. (SPI) with falsified test results were the likely cause of both of the OCO and Glory fairing failures.

Ground-Based Interceptor

The upper stages of the Minotaur-C are used by the boost vehicle of the Ground-Based Interceptor, the anti-ballistic missile component of the U.S. Missile Defense Agency's Ground-Based Midcourse Defense system.

See also

• Comparison of orbital launchers families
• Antares, an Orbital ATK rocket with a liquid first stage and a modified Castor 120 solid rocket as a second stage. Originally named Taurus II.
• Official fact sheet (2019)

External links

• Video of Minotaur-C launch on 31 October, 2017