KVD-1

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Initial development

Soviet crewed lunar programs Glavkosmos

2 related topics

Sanctions imposed by United States

Missile Technology Control Regime ISRO

2 related topics

ISRO programme

INSAT-4CR

1 related topics

Use

GSLV Mk I

1 related topics

Key facts & relationships

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Application: Upper stage engine
Associated LV: GSLV Mk 1
Burn time: 800 s (600 s in a single burn)
Chamber: 1 + 2 verniers
Chamber pressure: 5.6 MPa (810 psi)
Country of origin: Soviet Union · Russia

Topics to explore

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Overview

Russia
RD-56 RD-56?action=edit&redlink=1
N-1 N1 (rocket)

Initial development

ISRO programme

INSAT-4CR

Sanctions imposed by United States

Use

GSLV Mk I

Advanced semantic analysis

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Map overview Semantic statistics

Nodes15

Edges14

Triples44

Avg. degree1.87

Density0.133333

Components1

How this topic connects Entity context

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KVD-1

Top relations

related to Sanctions imposed by United States · 10

KVD-1 → But, Glavkosmos, In, India, ISRO, July, Missile Technology Control Regime, Russia, This, US

related to Initial development · 8

KVD-1 → Glavkosmos, ISRO, Later, N1, N1M, RD-56, Russia, Soviet

related to ISRO programme · 5

KVD-1 → Because, Later, Russian, The, The INSAT-4CR

Country of origin · 2

KVD-1 → Russia, Soviet Union

Application · 1

KVD-1 → Upper stage engine

Associated LV · 1

KVD-1 → GSLV Mk 1

Burn time · 1

KVD-1 → 800 s (600 s in a single burn)

Chamber · 1

KVD-1 → 1 + 2 verniers

Chamber pressure · 1

KVD-1 → 5.6 MPa (810 psi)

Cycle · 1

KVD-1 → Staged combustion

Important terminology Word statistics

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Important terminology

engine engines russia cryogenic isro upper stage developed mass thrust rd-56 used later rocket programme soviet ratio single kg kb

Entity relationships Subject–Predicate–Object triples

Subject	Predicate	Object	Confidence	Src
KVD-1	Application	Upper stage engine	1.00	infobox
KVD-1	Associated LV	GSLV Mk 1	1.00	infobox
KVD-1	Burn time	800 s (600 s in a single burn)	1.00	infobox
KVD-1	Chamber	1 + 2 verniers	1.00	infobox
KVD-1	Chamber pressure	5.6 MPa (810 psi)	1.00	infobox
KVD-1	Country of origin	Soviet Union	1.00	infobox
KVD-1	Country of origin	Russia	1.00	infobox
KVD-1	Cycle	Staged combustion	1.00	infobox
KVD-1	Designer	KB KhIMMASH	1.00	infobox
KVD-1	Diameter	1.58 m (5 ft 2 in)	1.00	infobox
KVD-1	Dry mass	282 kg (622 lb)	1.00	infobox
KVD-1	First flight	2001-04-20, GSAT-1 Mission, GSLV debut flight	1.00	infobox
KVD-1	Gimbal range	None; uses 2 vernier engines for attitude control	1.00	infobox
KVD-1	Last flight	2010-12-25, GSAT-5P launch, GSLV Mk I final flight	1.00	infobox
KVD-1	Length	2.14 m (7 ft 0 in)	1.00	infobox
KVD-1	Mixture ratio	6	1.00	infobox
KVD-1	Propellant	Liquid oxygen / liquid hydrogen	1.00	infobox
KVD-1	Specific impulse, vacuum	462 s	1.00	infobox
KVD-1	Status	Retired	1.00	infobox
KVD-1	Thrust, vacuum	69.6 kN (15,600 lbf)	1.00	infobox

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