Vikas (rocket engine)

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Explore the main themes, entities and connections around Vikas (rocket engine). Start with the topic map, then use the sections below for research and deeper semantic analysis.

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History

Societe Europeenne de Propulsion Nambi Narayanan KELTEC Brahmos Aerospace.

4 related topics

Technical details

UDMH Nitrogen tetroxide Gimballing GSAT 6A

4 related topics

Overview

Portmanteau VIKram Ambalal Sarabhai Liquid fuelled Rocket engines Liquid Propulsion Systems Centre

9 related topics

Key facts & relationships

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Chamber pressure: 6.2 MPa (62 bar)
Country of origin: India
Cycle: Gas generator
Designer: Société Européenne de Propulsion (SEP) · ISRO (licensed version)
Dry mass: 120 in (3,000 mm)
Length: 3.70 m (12.1 ft)(Vikas-4B)

Topics to explore

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Overview

History

Societe Europeenne de Propulsion
Nambi Narayanan
KELTEC Kerala Hitech Industries Limited
Brahmos Aerospace. BrahMos Aerospace

Technical details

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

Nodes21

Edges20

Triples14

Avg. degree1.9

Density0.095238

Components1

How this topic connects Entity context

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Vikas (rocket engine)

Top relations

Designer · 2

Vikas (rocket engine) → ISRO (licensed version), Société Européenne de Propulsion (SEP)

Chamber pressure · 1

Vikas (rocket engine) → 6.2 MPa (62 bar)

Country of origin · 1

Vikas (rocket engine) → India

Cycle · 1

Vikas (rocket engine) → Gas generator

Dry mass · 1

Vikas (rocket engine) → 120 in (3,000 mm)

Length · 1

Vikas (rocket engine) → 3.70 m (12.1 ft)(Vikas-4B)

Manufacturer · 1

Vikas (rocket engine) → Godrej & Boyce and MTAR Technologies

Predecessor · 1

Vikas (rocket engine) → Viking

Propellant · 1

Vikas (rocket engine) → N2O4 / UDMH

Specific impulse, sea-level · 1

Vikas (rocket engine) → 262 seconds (2.57 km/s)

Important terminology Word statistics

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

Important terminology

engine vikas lvm3 pslv gslv used propulsion version viking rocket engines isro thrust stage launch mark ii kn also licensed

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
Vikas (rocket engine)	Chamber pressure	6.2 MPa (62 bar)	1.00	infobox
Vikas (rocket engine)	Country of origin	India	1.00	infobox
Vikas (rocket engine)	Cycle	Gas generator	1.00	infobox
Vikas (rocket engine)	Designer	Société Européenne de Propulsion (SEP)	1.00	infobox
Vikas (rocket engine)	Designer	ISRO (licensed version)	1.00	infobox
Vikas (rocket engine)	Dry mass	120 in (3,000 mm)	1.00	infobox
Vikas (rocket engine)	Length	3.70 m (12.1 ft)(Vikas-4B)	1.00	infobox
Vikas (rocket engine)	Manufacturer	Godrej & Boyce and MTAR Technologies	1.00	infobox
Vikas (rocket engine)	Predecessor	Viking	1.00	infobox
Vikas (rocket engine)	Propellant	N2O4 / UDMH	1.00	infobox
Vikas (rocket engine)	Specific impulse, sea-level	262 seconds (2.57 km/s)	1.00	infobox
Vikas (rocket engine)	Specific impulse, vacuum	293 seconds (2.87 km/s)	1.00	infobox
Vikas (rocket engine)	Status	Active	1.00	infobox
Vikas (rocket engine)	Thrust	821 kN	1.00	infobox

Related concept clusters Concept neighborhoods

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