M-V

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Overview

Solid-fuel rocket Scientific Satellites Mu family Rockets

22 related topics

Comparable solid fuel rockets

Athena II Epsilon Minotaur IV Shavit Minotaur-C

6 related topics

Potential as an intercontinental ballistic missile

JAXA Threat from North Korea Tokyo Metropolitan Government Intercontinental ballistic missile LGM-118 Peacekeeper

5 related topics

Following program

H-IIA Hisaki

2 related topics

Key facts & relationships

High-confidence facts extracted from structured source data. Use them as anchors for further research.

Burn time: 46 seconds · 71 seconds · 102 seconds · 73 seconds
Carries passengers or cargo: HALCA, Nozomi, ASTRO-E, Hayabusa Suzaku, AKARI Hinode
Country of origin: Japan
Diameter: 2.5 m (8 ft 2 in)
Failure: 1 (M-V)
First flight: M-V: 10 February 2000 M-V KM: 12 February 1997

Topics to explore

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Overview

Solid-fuel rocket
Scientific Science
Satellites Satellite
Mu family Mu (rocket family)
Rockets Rocket
Institute of Space and Astronautical Science
Yen Japanese yen
Diameter
Orbit
HALCA
Radio astronomy
Nozomi Mars explorer Nozomi (spacecraft)
Astro-E
X-ray
Hayabusa
25143 Itokawa
Astro-E2 Suzaku (satellite)
Hinode Hinode (satellite)
SSSat SSSat?action=edit&redlink=1
Microsat Miniaturized satellite
Nanosatellite
HIT-SAT HIT-SAT?action=edit&redlink=1

Following program

H-IIA
Hisaki Hisaki (satellite)

Potential as an intercontinental ballistic missile

JAXA
Threat from North Korea North Korea and weapons of mass destruction
Tokyo Metropolitan Government
Intercontinental ballistic missile
LGM-118 Peacekeeper

Comparable solid fuel rockets

Athena II
Epsilon Epsilon (rocket)
Minotaur IV
Shavit Shavit 2
Minotaur-C
Vega Vega (rocket)

Advanced semantic analysis

Deeper signals for content research, entity SEO and topical coverage. The plain-language headings explain what each technical view is useful for.

Map overview Semantic statistics

Nodes40

Edges39

Triples46

Avg. degree1.95

Density0.05

Components1

How this topic connects Entity context

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M-V

Top relations

related to Following program · 9

M-V → Epsilon, Epsilon Rocket, H-IIA, Hisaki, LEO, September, SPRINT-A, The, US

related to External links · 6

M-V → Encyclopedia Astronautica, ISAS, JAXA Archived, JAXAM-V, March, Wayback MachineEpsilon Launch Vehicle

Burn time · 4

M-V → 102 seconds, 46 seconds, 71 seconds, 73 seconds

Maximum thrust · 4

M-V → 1,245.287 kN (279,952 lbf), 294 kN (66,000 lbf), 3,780.345 kN (849,855 lbf), 51.9 kN (11,700 lbf)

Specific impulse · 4

M-V → 203 s (1.99 km/s), 246 s (2.41 km/s), 298 s (2.92 km/s), 301 s (2.95 km/s)

Mass · 3

M-V → 1,300 kg (2,900 lb), 1,800 kg (4,000 lb), 137,500–139,000 kg (303,100–306,400 lb)

Carries passengers or cargo · 1

M-V → HALCA, Nozomi, ASTRO-E, Hayabusa Suzaku, AKARI Hinode

Country of origin · 1

M-V → Japan

Diameter · 1

M-V → 2.5 m (8 ft 2 in)

Failure · 1

M-V → 1 (M-V)

Important terminology Word statistics

Use these terms to understand the vocabulary surrounding the topic, not as a checklist for keyword stuffing.

Important terminology

launch rocket satellite isas astro-e scientific first 000 kg lb solid hayabusa epsilon launches rockets also halca hinode high launched

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
M-V	Burn time	46 seconds	1.00	infobox
M-V	Burn time	71 seconds	1.00	infobox
M-V	Burn time	102 seconds	1.00	infobox
M-V	Burn time	73 seconds	1.00	infobox
M-V	Carries passengers or cargo	HALCA, Nozomi, ASTRO-E, Hayabusa Suzaku, AKARI Hinode	1.00	infobox
M-V	Country of origin	Japan	1.00	infobox
M-V	Diameter	2.5 m (8 ft 2 in)	1.00	infobox
M-V	Failure	1 (M-V)	1.00	infobox
M-V	First flight	M-V: 10 February 2000 M-V KM: 12 February 1997	1.00	infobox
M-V	Function	All-solid small orbital launch vehicle	1.00	infobox
M-V	Height	30.8 m (101 ft)	1.00	infobox
M-V	Last flight	M-V: 22 September 2006 M-V KM: 9 May 2003	1.00	infobox
M-V	Launch sites	Uchinoura M-V	1.00	infobox
M-V	Manufacturer	Nissan Motors (-2000) IHI AEROSPACE (-2006)	1.00	infobox
M-V	Mass	137,500–139,000 kg (303,100–306,400 lb)	1.00	infobox
M-V	Mass	1,800 kg (4,000 lb)	1.00	infobox
M-V	Mass	1,300 kg (2,900 lb)	1.00	infobox
M-V	Maximum thrust	3,780.345 kN (849,855 lbf)	1.00	infobox
M-V	Maximum thrust	1,245.287 kN (279,952 lbf)	1.00	infobox
M-V	Maximum thrust	294 kN (66,000 lbf)	1.00	infobox
M-V	Maximum thrust	51.9 kN (11,700 lbf)	1.00	infobox
M-V	Powered by	1 solid	1.00	infobox
M-V	Propellant	Solid	1.00	infobox
M-V	Specific impulse	246 s (2.41 km/s)	1.00	infobox
M-V	Specific impulse	203 s (1.99 km/s)	1.00	infobox
M-V	Specific impulse	301 s (2.95 km/s)	1.00	infobox
M-V	Specific impulse	298 s (2.92 km/s)	1.00	infobox
M-V	Stages	3 or 4	1.00	infobox
M-V	Status	Retired	1.00	infobox
M-V	Success(es)	6 (M-V: 3, M-V KM: 3)	1.00	infobox

Related concept clusters Concept neighborhoods

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Connections between topic areas Semantic bridges

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