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AJ10

The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet). It has been used to propel the upper stages of several launch vehicles, including the Delta II and Titan III. Variants were and are used as the service propulsion engine for the Apollo command and service module, in the Space Shuttle Orbital Maneuvering…

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Application
Upper stage
Chamber
1
Chamber pressure
7–9 bars (700–900 kPa)
Country of origin
United States
Cycle
Pressure-fed
Date
1957–present

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Overview

Variants

Advanced semantic analysis

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Map overview Semantic statistics

AJ10

Nodes35
Edges34
Triples78
Avg. degree1.94
Density0.057143
Components1

How this topic connects Entity context

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AJ10

Top relations

related to AJ10-190 · 12
AJ10 → CH6N2, Following, Isp, N2O4, OMS, Orion, Shuttle, Space Shuttle Orbital Maneuvering, System, The AJ10-190, They, This
related to AJ10-118F · 10
AJ10 → Aerozine, AJ10-138, Delta, Delta-F, It, N2O4, Straight Eight, The AJ10-118F, This, Transtage
related to AJ10-101 · 9
AJ10 → Able, AJ10-101, April, Atlas-Able, July, The, The AJ10-101, Thor, Thor-Able
related to AJ10-37 · 9
AJ10 → AJ10-37, An AJ10, Delta-A/Able, HNO3, It, March, The AJ10, UDMH, Vanguard
related to AJ10-118K · 8
AJ10 → Aerozine, Delta II, Delta-K, ICESat-2, It, N2O4, September, The AJ10-118K
related to AJ10-137 · 7
AJ10 → Aerozine, Apollo, N2O4, The AJ10-137, This, Trans-Earth, UDMH
related to AJ10-138 · 5
AJ10 → Able, The AJ10-138, Titan III GTO Transtage, Two, Vanguard
Propellant · 4
AJ10 → .mw-parser-output .template-chem2-su{display:inline-block;font-size:80%;line-height:1;vertical-align:-0.35em}.mw-parser-output .template-chem2-suspan{display:block;text-align:l…, HNO3 / Aniline, N2O4 / Aerozine-50, N2O4 / CH6N2
Application · 1
AJ10 → Upper stage
Chamber · 1
AJ10 → 1

Important terminology Word statistics

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Important terminology

used engine stage upper first n2o4 able apollo thrust lbf delta service shuttle system orion oxidizer aj10-118k vanguard ii aj10-101

Entity relationships Subject–Predicate–Object triples

SubjectPredicateObjectConfidenceSrc
AJ10ApplicationUpper stage1.00infobox
AJ10Chamber11.00infobox
AJ10Chamber pressure7–9 bars (700–900 kPa)1.00infobox
AJ10Country of originUnited States1.00infobox
AJ10CyclePressure-fed1.00infobox
AJ10Date1957–present1.00infobox
AJ10Diameter0.84 m (2 ft 9 in)1.00infobox
AJ10Dry mass90–100 kg (200–220 lb)1.00infobox
AJ10ManufacturerAerojet Aerojet Rocketdyne1.00infobox
AJ10Propellant.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…1.00infobox
AJ10PropellantHNO3 / Aniline1.00infobox
AJ10PropellantN2O4 / Aerozine-501.00infobox
AJ10PropellantN2O4 / CH6N21.00infobox
AJ10Specific impulse, vacuum270–319 seconds (2.65–3.13 km/s)1.00infobox
AJ10StatusIn use1.00infobox
AJ10Thrust, vacuum43.7 kN (9,800 lbf)1.00infobox
AJ10is ahypergolic rocket engine manufactured by Aerojet Rocketdyne0.90text

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