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OPd-56-39-22D
Part of Stromboli
French test vehicle. Original designation of the Antares test vehicle.

Status: Retired 1960. First Launch: 1959-05-02. Last Launch: 1960-09-30. Number: 7 . Thrust: 200.00 kN (44,960 lbf). Gross mass: 1,800 kg (3,900 lb). Height: 12.20 m (40.00 ft). Diameter: 0.56 m (1.83 ft). Apogee: 280 km (170 mi).

4 stage vehicle consisting of 1 x Vesuve + 1 x Neptune + 1 x Mimosa + 1 x Melanie.

Subtopics
Neptune engine ONERA solid rocket engine. Second stage of OPd-56-39-22D vehicle.
SEPR 685-4 ONERA solid rocket engine. OPd-56-39-22D third stage.
Family: test vehicle. Country: France. Launch Sites: Ile du Levant. Stages: Neptune engine, SEPR 685-4, Melanie, SEPR 734-1. Agency: ONERA.
1959 May 2 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Stromboli. Launch Vehicle: OPd-56-39-22D.
1959 October 22 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Stromboli. Launch Vehicle: OPd-56-39-22D.
1959 December 15 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Stromboli. Launch Vehicle: OPd-56-39-22D.
1960 May 2 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Stromboli. Launch Vehicle: OPd-56-39-22D.
1960 May 5 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Stromboli. Launch Vehicle: OPd-56-39-22D.
1960 September 26 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Stromboli. Launch Vehicle: OPd-56-39-22D.
1960 September 30 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Stromboli. Launch Vehicle: OPd-56-39-22D.
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