Nitric acid/Turpentine

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Nitric acid/Turpentine

Nitric acid/Turpentine propellant. Combination used in early test rockets; no production engines resulted.

Subtopics

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.

Veronique 61 engine LRBA Nitric acid/Turpentine rocket engine.

Veronique 61 stage Nitric acid/Turpentine propellant rocket stage.

Veronique 61M stage Nitric acid/Turpentine propellant rocket stage.

Veronique AGI engine LRBA Nitric acid/Turpentine rocket engine.

Veronique AGI stage Nitric acid/Turpentine rocket stage. 40.00 kN (8,992 lbf) thrust. Mass 1,300 kg (2,866 lb).

Vesta-1 Nitric acid/Turpentine rocket stage. 140.00 kN (31,473 lbf) thrust. Mass 5,000 kg (11,023 lb).

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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