RD-856

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Explore the main themes, entities and connections around RD-856. Start with the topic map, then use the sections below for research and deeper semantic analysis.

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Overview

Russian Romanized Lit.GRAU index Liquid-fuel

18 related topics

Key facts & relationships

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

Application: Vernier
Associated LV: R-36, Tsyklon-2 and Tsyklon-3
Burn time: Up to 163 s
Chamber: 4
Chamber pressure: 7.160 MPa (1,038.5 psi)
Country of origin: Soviet Union

Topics to explore

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Overview

Russian Russian language
Romanized Romanization of Russian
Lit. Literal translation
GRAU index
Liquid-fuel Liquid-fuel rocket
Rocket Rocket engine
Vernier engine Vernier thruster
Hypergolic Hypergolic propellant
Unsymmetrical dimethylhydrazine
Dinitrogen tetroxide
Gas generator cycle Gas-generator cycle (rocket)
R-36 R-36 (missile)
Tsyklon-2
Tsyklon-3
Thrust vector control Thrust vectoring
Gimbaling Gimbaled thrust
RD-252
Tsyklon-4

Advanced semantic analysis

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Map overview Semantic statistics

Nodes20

Edges19

Triples30

Avg. degree1.9

Density0.1

Components1

How this topic connects Entity context

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RD-856

Top relations

see also · 9

RD-856 → R-36, Soviet, The RD-856, The Soviet ICBM, Tsyklon-2, Tsyklon-3, Tsyklon-4, Ukrainian, Yuzhnoe Design Bureau

Application · 1

RD-856 → Vernier

Associated LV · 1

RD-856 → R-36, Tsyklon-2 and Tsyklon-3

Burn time · 1

RD-856 → Up to 163 s

Chamber · 1

RD-856 → 4

Chamber pressure · 1

RD-856 → 7.160 MPa (1,038.5 psi)

Country of origin · 1

RD-856 → Soviet Union

Cycle · 1

RD-856 → Gas generator

Designer · 1

RD-856 → Yuzhnoye Design Bureau

Diameter · 1

RD-856 → 3.35 m (11.0 ft)

Important terminology Word statistics

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

Important terminology

engine r-36 tsyklon-3 soviet tsyklon-2 rocket structure 1965 udmh also tsyklon-4 design bureau vernier mixture n2o4 gas generator cycle second

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
RD-856	Application	Vernier	1.00	infobox
RD-856	Associated LV	R-36, Tsyklon-2 and Tsyklon-3	1.00	infobox
RD-856	Burn time	Up to 163 s	1.00	infobox
RD-856	Chamber	4	1.00	infobox
RD-856	Chamber pressure	7.160 MPa (1,038.5 psi)	1.00	infobox
RD-856	Country of origin	Soviet Union	1.00	infobox
RD-856	Cycle	Gas generator	1.00	infobox
RD-856	Designer	Yuzhnoye Design Bureau	1.00	infobox
RD-856	Diameter	3.35 m (11.0 ft)	1.00	infobox
RD-856	Dry mass	112.5 kg (248 lb)	1.00	infobox
RD-856	First flight	December 16, 1965	1.00	infobox
RD-856	Gimbal range	±30°	1.00	infobox
RD-856	Last flight	January 30, 2009	1.00	infobox
RD-856	Length	0.9 m (2 ft 11 in)	1.00	infobox
RD-856	Manufacturer	Yuzhmash	1.00	infobox
RD-856	Mixture ratio	1.98	1.00	infobox
RD-856	Propellant	.mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-su>span{display:block;text-align:l…	1.00	infobox
RD-856	Restarts	1	1.00	infobox
RD-856	Specific impulse, vacuum	280.5 s (2.751 km/s)	1.00	infobox
RD-856	Status	Out of production	1.00	infobox
RD-856	Thrust, vacuum	54.23 kN (12,190 lbf)	1.00	infobox

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