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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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used engine stage upper first n2o4 able apollo thrust lbf delta service shuttle system orion oxidizer aj10-118k vanguard ii aj10-101
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| AJ10 | Application | Upper stage | 1.00 | infobox |
| AJ10 | Chamber | 1 | 1.00 | infobox |
| AJ10 | Chamber pressure | 7–9 bars (700–900 kPa) | 1.00 | infobox |
| AJ10 | Country of origin | United States | 1.00 | infobox |
| AJ10 | Cycle | Pressure-fed | 1.00 | infobox |
| AJ10 | Date | 1957–present | 1.00 | infobox |
| AJ10 | Diameter | 0.84 m (2 ft 9 in) | 1.00 | infobox |
| AJ10 | Dry mass | 90–100 kg (200–220 lb) | 1.00 | infobox |
| AJ10 | Manufacturer | Aerojet Aerojet Rocketdyne | 1.00 | infobox |
| AJ10 | 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 |
| AJ10 | Propellant | HNO3 / Aniline | 1.00 | infobox |
| AJ10 | Propellant | N2O4 / Aerozine-50 | 1.00 | infobox |
| AJ10 | Propellant | N2O4 / CH6N2 | 1.00 | infobox |
| AJ10 | Specific impulse, vacuum | 270–319 seconds (2.65–3.13 km/s) | 1.00 | infobox |
| AJ10 | Status | In use | 1.00 | infobox |
| AJ10 | Thrust, vacuum | 43.7 kN (9,800 lbf) | 1.00 | infobox |
| AJ10 | is a | hypergolic rocket engine manufactured by Aerojet Rocketdyne | 0.90 | text |
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