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M-V: Science, Overview & Comparable solid fuel rockets

The M-V rocket, also called M-5 or Mu-5, was a Japanese solid-fuel rocket designed to launch scientific satellites. It was a member of the Mu family of rockets. The Institute of Space and Astronautical Science (ISAS) began developing the M-V in 1990 at a cost of 15 billion yen. It has three stages and is 30.7 m (101 ft) high, 2.5 m (8 ft 2 in) in…

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M-V topic overview

The analysis highlights Science, Overview and Comparable solid fuel rockets as prominent areas in the source structure around M-V.

Related topics
35
Source areas
4
Connected nodes
39
Extracted relationships
46
Concept neighborhoods
16
Bridge connections
39

What this topic covers Research coverage

Source areas are shown by the number of related topics found in each part of the analysis. Use smaller areas too: they can reveal specialized angles and content gaps.

Overview · 22 topics
Comparable solid fuel rockets · 6 topics
Potential as an intercontinental ballistic missile · 5 topics
Following program · 2 topics

Smaller areas are not necessarily less important. They contain fewer connections in this analysis and can be useful for finding specialized angles or coverage gaps.

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

Explore all related topics Closing gaps

Browse the complete topic structure, not only the most central items. Less prominent entities and concepts can reveal missing angles, specialized context and useful research gaps. Each item opens a new analysis centered on that subject.

Overview

Following program

Potential as an intercontinental ballistic missile

Comparable solid fuel rockets

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.

How M-V connects Entity context

The extracted context around M-V shows recurring relationship patterns in the source. For example, M-V → Epsilon, Epsilon Rocket, H-IIA, Hisaki, LEO, September, SPRINT-A, The, US Another extracted example is M-V → Encyclopedia Astronautica, ISAS, JAXA Archived, JAXAM-V, March, Wayback MachineEpsilon Launch Vehicle. Use these groups to spot repeated connection types before inspecting the individual relationships.

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

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

M-V relationships Subject–Predicate–Object triples

TTTA extracted 46 structured relationships around M-V. Examples in this analysis include M-V → Burn time → 46 seconds and M-V → Burn time → 71 seconds. The table shows each extracted connection, where it came from and its confidence.

SubjectPredicateObjectConfidenceSrc
M-VBurn time46 seconds1.00infobox
M-VBurn time71 seconds1.00infobox
M-VBurn time102 seconds1.00infobox
M-VBurn time73 seconds1.00infobox
M-VCarries passengers or cargoHALCA, Nozomi, ASTRO-E, Hayabusa Suzaku, AKARI Hinode1.00infobox
M-VCountry of originJapan1.00infobox
M-VDiameter2.5 m (8 ft 2 in)1.00infobox
M-VFailure1 (M-V)1.00infobox
M-VFirst flightM-V: 10 February 2000 M-V KM: 12 February 19971.00infobox
M-VFunctionAll-solid small orbital launch vehicle1.00infobox
M-VHeight30.8 m (101 ft)1.00infobox
M-VLast flightM-V: 22 September 2006 M-V KM: 9 May 20031.00infobox
M-VLaunch sitesUchinoura M-V1.00infobox
M-VManufacturerNissan Motors (-2000) IHI AEROSPACE (-2006)1.00infobox
M-VMass137,500–139,000 kg (303,100–306,400 lb)1.00infobox
M-VMass1,800 kg (4,000 lb)1.00infobox
M-VMass1,300 kg (2,900 lb)1.00infobox
M-VMaximum thrust3,780.345 kN (849,855 lbf)1.00infobox
M-VMaximum thrust1,245.287 kN (279,952 lbf)1.00infobox
M-VMaximum thrust294 kN (66,000 lbf)1.00infobox
M-VMaximum thrust51.9 kN (11,700 lbf)1.00infobox
M-VPowered by1 solid1.00infobox
M-VPropellantSolid1.00infobox
M-VSpecific impulse246 s (2.41 km/s)1.00infobox
M-VSpecific impulse203 s (1.99 km/s)1.00infobox
M-VSpecific impulse301 s (2.95 km/s)1.00infobox
M-VSpecific impulse298 s (2.92 km/s)1.00infobox
M-VStages3 or 41.00infobox
M-VStatusRetired1.00infobox
M-VSuccess(es)6 (M-V: 3, M-V KM: 3)1.00infobox

Related concept clusters Concept neighborhoods

The concept neighborhoods around M-V bring nearby vocabulary together. In this analysis, examples include Launch, Ballistic and Missile. Use the clusters to find adjacent concepts and terminology that may deserve separate research.

  • M-V
    • Launch
    • Ballistic
    • Missile
    • Epsilon
    • Launches
    • Rocket
    • Astro-eii
    • Called
    • Following
    • Halca
    • July
    • Nozomi
  • m-v
    • Launch
    • Ballistic
    • Missile
    • Epsilon
    • Launches
    • Rocket
    • Astro-eii
    • Called
    • Following
    • Halca
    • July
    • Nozomi
  • solid-fuel rocket
    • Also
    • First
    • Called
    • Halca
    • Nozomi
    • Rocket
    • Solid-fuel
    • Astro-e
    • Scientific
    • Solid
    • Satellite
    • Isas
  • astro-e
    • Satellite
    • Rocket
    • Launch
    • Astro-eii
    • Called
    • Diameter
    • Following
    • Ft
    • Halca
    • Hinode
    • July
    • Km
  • diameter
    • Ft
    • Stages
    • Kg
    • Lb
    • Astro-eii
    • Halca
    • High
    • Hinode
    • Km
    • Nozomi
    • Astro-e
    • Capability
  • halca
    • Nozomi
    • Astro-eii
    • Hinode
    • July
    • Km
    • Launched
    • Rocket
    • Stages
    • Astro-e
    • Capability
    • Hayabusa
    • Kg
  • hayabusa
    • Capability
    • Astro-eii
    • Hinode
    • Km
    • Launched
    • Nozomi
    • Stages
    • Ballistic
    • Kg
    • Lb
    • Missile
    • Payload
  • epsilon
    • Launches
    • Capability
    • Payload
    • Launch
    • M-v
    • Ft
    • Halca
    • Hinode
    • Km
    • Nozomi
    • Stages
    • Hayabusa

Connections between topic areas Semantic bridges

For M-V, one of the stronger structural bridges in this analysis connects M-V with Overview. Bridges highlight paths between different parts of the map and can reveal research angles that are easy to miss in a flat list.

Min side: 3
M-VOverview · splits 17 ⟂ 23
M-VComparable solid fuel rockets · splits 33 ⟂ 7
M-VPotential as an intercontinental ballistic missile · splits 34 ⟂ 6
M-VFollowing program · splits 37 ⟂ 3

Map overview Semantic statistics

M-V

Nodes40
Edges39
Triples46
Avg. degree1.95
Density0.05
Components1

Source & methodology

TTTA analyzes the structure around M-V to surface related topics, entities, relationships, concept neighborhoods and bridge connections. Use the map to explore areas such as Science, Overview & Comparable solid fuel rockets, including less central topics that may reveal useful research gaps. Automatically extracted connections are research leads rather than rewritten encyclopedia content.

Source: Wikipedia — M-V · EN edition · Analysis: TopicsToTalkAbout

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