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VE10 Aigle

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VE10 Aigle
Part of Stromboli Family
The Aigle's simple mission was to allow test of the telemetry equipment that would be used on later instrumented warheads. The first version of the Aigle was a simple fin-stabilized solid rocket propelled by a Stromboli SEPR 737 loaded with 984 kg of 'Plastolite' propellant.
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AKA: Aigle VE10. Status: Retired 1961. First Launch: 1960-12-17. Last Launch: 1961-03-21. Number: 4 . Payload: 360 kg (790 lb). Gross mass: 2,300 kg (5,000 lb). Height: 8.00 m (26.20 ft). Diameter: 0.55 m (1.80 ft). Apogee: 20 km (12 mi).

Payload: 360 kg (790 lb) to a 20 km altitude.

Family: test vehicle. Country: France. Launch Sites: Hammaguira, Hammaguira Bacchus. Stages: SEPR 737. Agency: SEREB.

1960 December 17 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. LV Family: Stromboli. Launch Vehicle: VE10 Aigle.
  • Test mission - . Nation: France. Agency: ONERA. Apogee: 20 km (12 mi).
1960 December 19 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. LV Family: Stromboli. Launch Vehicle: VE10 Aigle.
  • Test mission - . Nation: France. Agency: ONERA. Apogee: 20 km (12 mi).
1961 March 16 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. LV Family: Stromboli. Launch Vehicle: VE10 Aigle.
  • Test mission - . Nation: France. Agency: ONERA. Apogee: 20 km (12 mi).
1961 March 21 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. LV Family: Stromboli. Launch Vehicle: VE10 Aigle.
  • Test mission - . Nation: France. Agency: ONERA. Apogee: 20 km (12 mi).
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