Nitric acid/Turpentine (original) (raw)
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Nitric acid/Turpentine
Nitric acid/Turpentine propellant. Combination used in early test rockets; no production engines resulted.
Subtopics
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Veronique After the cancellation of the 'Super V-2' project, the German team at Vernon pursued development of a tenth-scale version, the Project 4213 Veronique (VERnon et electrONIQUE). The 4 metric ton thrust motor, using nitric acid and kerosene, beat the 'pure French' project 4211 Eole design and paved the way leading to the Ariane space booster. |
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| Veronique AGI stage Nitric acid/Turpentine rocket stage. 40.00 kN (8,992 lbf) thrust. Mass 1,300 kg (2,866 lb). |
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| Vesta-1 Nitric acid/Turpentine rocket stage. 140.00 kN (31,473 lbf) thrust. Mass 5,000 kg (11,023 lb). |
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Engines: Veronique 61 engine, Veronique AGI engine. Launch Vehicles: Veronique. Stages: Veronique 61 stage, Veronique AGI stage, Vesta-1, Veronique 61M stage.
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