Minotaur-C

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Explore the main themes, entities and connections around Minotaur-C. Start with the topic map, then use the sections below for research and deeper semantic analysis.

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Launch failures

Orbiting Carbon Observatory 2 Delta II Vermont Composites Ensign-Bickford Company MIB

6 related topics

Stages

Castor 120 Peacekeeper Orion 38 Delta

4 related topics

Ground-Based Interceptor

Ground-Based Interceptor Anti-ballistic missile Ground-Based Midcourse Defense

3 related topics

Overview

Stage Solid fueled Launch vehicle Orbital Sciences Northrop Grumman

12 related topics

Key facts & relationships

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Based on: Pegasus
Burn time: 83 seconds · 73 seconds · 65 seconds
Cost per launch: US$40−50 million (2017)
Country of origin: United States
Diameter: 2.35 m (7 ft 9 in)[citation needed]
Failure: 3

Topics to explore

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Overview

Stage Multistage rocket
Solid fueled Solid rocket
Launch vehicle
Orbital Sciences Orbital Sciences Corporation
Northrop Grumman
SLC-576E
Vandenberg Air Force Base
Pegasus Northrop Grumman Pegasus
Low Earth orbit
Orbiting Carbon Observatory
Glory Glory (satellite)
Minotaur Minotaur (rocket family)

Stages

Castor 120 Castor (rocket stage)
Peacekeeper LGM-118 Peacekeeper
Orion 38 Orion (rocket stage)
Delta Delta (rocket family)

Launch failures

Orbiting Carbon Observatory 2
Delta II
Vermont Composites Vermont Composites?action=edit&redlink=1
Ensign-Bickford Company
MIB Mishap Investigation Board?action=edit&redlink=1
Sapa Profiles

Ground-Based Interceptor

Advanced semantic analysis

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Map overview Semantic statistics

Nodes30

Edges29

Triples46

Avg. degree1.93

Density0.066667

Components1

How this topic connects Entity context

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Minotaur-C

Top relations

related to Stages · 7

Minotaur-C → Orbital ATK Castor, Orion, Orion-50s, Peacekeeper ICBM, Pegasus, Stages, The Minotaur-C's

Maximum thrust · 4

Minotaur-C → 1,606.6 kN (361,200 lbf), 118.2 kN (26,600 lbf), 34.57 kN (7,770 lbf), 484.9 kN (109,000 lbf)

Specific impulse · 4

Minotaur-C → 285 s (2.79 km/s), 286 s (2.80 km/s), 292 s (2.86 km/s), 293 s (2.87 km/s)

related to Ground-Based Interceptor · 4

Minotaur-C → Ground-Based Interceptor, Midcourse Defense, Missile Defense Agency's Ground-Based, The

Burn time · 3

Minotaur-C → 65 seconds, 73 seconds, 83 seconds

Manufacturer · 3

Minotaur-C → Northrop Grumman (2018–present), Orbital ATK (2015–2018), Orbital Sciences (1994–2015)

Mass · 3

Minotaur-C → 1,054 kg (2,324 lb), 1,458 kg (3,214 lb), 73,000 kg (161,000 lb)[citation needed]

related to External links · 2

Minotaur-C → October, Video

Based on · 1

Minotaur-C → Pegasus

Cost per launch · 1

Minotaur-C → US$40−50 million (2017)

Important terminology Word statistics

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Important terminology

launch stage taurus rocket vehicle glory orbital failure million xl system first us based minotaur stages fairing failed used orbiting

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
Minotaur-C	Based on	Pegasus	1.00	infobox
Minotaur-C	Burn time	83 seconds	1.00	infobox
Minotaur-C	Burn time	73 seconds	1.00	infobox
Minotaur-C	Burn time	65 seconds	1.00	infobox
Minotaur-C	Cost per launch	US$40−50 million (2017)	1.00	infobox
Minotaur-C	Country of origin	United States	1.00	infobox
Minotaur-C	Diameter	2.35 m (7 ft 9 in)[citation needed]	1.00	infobox
Minotaur-C	Failure	3	1.00	infobox
Minotaur-C	Family	Minotaur	1.00	infobox
Minotaur-C	First flight	13 March 1994	1.00	infobox
Minotaur-C	Function	Small-lift launch vehicle	1.00	infobox
Minotaur-C	Height	27.9 m (92 ft)[citation needed]	1.00	infobox
Minotaur-C	Last flight	13 October 2017	1.00	infobox
Minotaur-C	Launch sites	Vandenberg, SLC-576E	1.00	infobox
Minotaur-C	Manufacturer	Orbital Sciences (1994–2015)	1.00	infobox
Minotaur-C	Manufacturer	Orbital ATK (2015–2018)	1.00	infobox
Minotaur-C	Manufacturer	Northrop Grumman (2018–present)	1.00	infobox
Minotaur-C	Mass	73,000 kg (161,000 lb)[citation needed]	1.00	infobox
Minotaur-C	Mass	1,458 kg (3,214 lb)	1.00	infobox
Minotaur-C	Mass	1,054 kg (2,324 lb)	1.00	infobox
Minotaur-C	Maximum thrust	1,606.6 kN (361,200 lbf)	1.00	infobox
Minotaur-C	Maximum thrust	484.9 kN (109,000 lbf)	1.00	infobox
Minotaur-C	Maximum thrust	118.2 kN (26,600 lbf)	1.00	infobox
Minotaur-C	Maximum thrust	34.57 kN (7,770 lbf)	1.00	infobox
Minotaur-C	Propellant	HTPB / Al	1.00	infobox
Minotaur-C	Specific impulse	286 s (2.80 km/s)	1.00	infobox
Minotaur-C	Specific impulse	285 s (2.79 km/s)	1.00	infobox
Minotaur-C	Specific impulse	292 s (2.86 km/s)	1.00	infobox
Minotaur-C	Specific impulse	293 s (2.87 km/s)	1.00	infobox
Minotaur-C	Stages	4	1.00	infobox

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