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Pegasus was an air-launched, small-lift launch vehicle developed by Orbital Sciences Corporation and later built and launched by Northrop Grumman. Pegasus was the world's first privately developed orbital launch vehicle. Capable of carrying small payloads of up to 443 kilograms (977 lb) into low Earth orbit, Pegasus first flew in 1990 and last flew…
The analysis highlights History, Art, Science and Companies as prominent areas in the source structure around Northrop Grumman Pegasus.
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.
Each route connects two topics through a shared source area. It is a way to explore, not a claim of a direct relationship.
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 Northrop Grumman Pegasus shows recurring relationship patterns in the source. For example, Northrop Grumman Pegasus → 131 + 110 seconds (2 burns), 68.5 seconds, 68.6 seconds, 69.4 seconds, 75.3 seconds, 75.6 seconds Another extracted example is Northrop Grumman Pegasus → 0.666 kN (150 lbf), 114.6 kN (25,800 lbf), 196 kN (44,171 lbf), 36 kN (8,062 lbf), 500 kN (110,000 lbf), 726 kN (163,247 lbf). 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 57 structured relationships around Northrop Grumman Pegasus. Examples in this analysis include Northrop Grumman Pegasus → Altitude → 200 km (120 mi) and Northrop Grumman Pegasus → Burn time → 75.3 seconds. The table shows each extracted connection, where it came from and its confidence.
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Northrop Grumman Pegasus | Altitude | 200 km (120 mi) | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 75.3 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 68.6 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 75.6 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 69.4 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 68.5 seconds | 1.00 | infobox |
| Northrop Grumman Pegasus | Burn time | 131 + 110 seconds (2 burns) | 1.00 | infobox |
| Northrop Grumman Pegasus | Comparable | Electron, Vector-H, Falcon 1, LauncherOne | 1.00 | infobox |
| Northrop Grumman Pegasus | Cost per launch | US$40 million (2017) | 1.00 | infobox |
| Northrop Grumman Pegasus | Country of origin | United States | 1.00 | infobox |
| Northrop Grumman Pegasus | Derivative work | Minotaur-C | 1.00 | infobox |
| Northrop Grumman Pegasus | Diameter | 1.28 m (4 ft 2 in) Wing span: 6.7 m (22 ft) | 1.00 | infobox |
| Northrop Grumman Pegasus | Diameter | 0.97 m (3 ft 2 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Empty mass | 1,369 kg (3,018 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Empty mass | 416 kg (917 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Empty mass | 126 kg (278 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Failure | 3 | 1.00 | infobox |
| Northrop Grumman Pegasus | First flight | April 5, 1990 (Pegsat / NavySat) | 1.00 | infobox |
| Northrop Grumman Pegasus | Function | Small-lift launch vehicle | 1.00 | infobox |
| Northrop Grumman Pegasus | Gross mass | 16,383 kg (36,118 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Gross mass | 4,341 kg (9,570 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Gross mass | 872.3 kg (1,923 lb) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | Standard: 16.9 m (55 ft 5 in) XL: 17.6 m (57 ft 9 in): 3 | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 10.27 m (33 ft 8 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 3.11 m (10 ft 2 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 1.34 m (4 ft 5 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Height | 0.3 m (1 ft 0 in) | 1.00 | infobox |
| Northrop Grumman Pegasus | Last flight | July 3, 2026 (Swift rescue mission (LINK)) | 1.00 | infobox |
| Northrop Grumman Pegasus | Launch sites | Air launch to orbit from Cape Canaveral, Edwards, Gando, Kennedy, Kwajalein, Vandenberg or Wallops | 1.00 | infobox |
| Northrop Grumman Pegasus | Manufacturer | Orbital Sciences (1990–2015) | 1.00 | infobox |
The concept neighborhoods around Northrop Grumman Pegasus bring nearby vocabulary together. In this analysis, examples include Grumman, Northrop and Sciences. Use the clusters to find adjacent concepts and terminology that may deserve separate research.
For Northrop Grumman Pegasus, one of the stronger structural bridges in this analysis connects Northrop Grumman Pegasus with History. 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 Northrop Grumman Pegasus to surface related topics, entities, relationships, concept neighborhoods and bridge connections. Use the map to explore areas such as History, Art, Science & Companies, including less central topics that may reveal useful research gaps. Automatically extracted connections are research leads rather than rewritten encyclopedia content.
Source: Wikipedia — Northrop Grumman Pegasus · EN edition · Analysis: TopicsToTalkAbout