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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…
The analysis highlights Science, Overview and Comparable solid fuel rockets as prominent areas in the source structure around M-V.
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.
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.
High-confidence facts extracted from structured source data. Use them as anchors for further research.
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.
Deeper signals for content research, entity SEO and topical coverage. The plain-language headings explain what each technical view is useful for.
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.
Use these terms to understand the vocabulary surrounding the topic, not as a checklist for keyword stuffing.
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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.
| 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 |
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.
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.
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