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Antares
Series of Thiokol solid rocket engines used on the Scout launch vehicle.



Subtopics

Antares 1A Thiokol solid rocket engine. Used on Blue Scout 1, Blue Scout 2, Blue Scout Junior, Scout X-1. First flight 1960.

Antares 2 Thiokol solid rocket engine. Used on Scout A, Scout B, Scout D, Scout F, Scout X-2, Scout X-3, Scout X-4. First flight 1962.

Antares 3 Thiokol solid rocket engine. In Production. Antares III, third-generation third stage for Scout launch vehicle. Propellant: AP/HTPB/Al propellant in a filament wound Kevlar case.

Antares 3A Thiokol solid rocket engine. Out of production. Used on Scout G launch vehicle. First flight 1979.



1960 November 25 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Antares.
  • Re-entry Vehicle test - . Nation: France. Agency: ONERA. Apogee: 150 km (90 mi).

1960 November 30 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Antares.
  • Re-entry Vehicle test - . Nation: France. Agency: ONERA. Apogee: 150 km (90 mi).

1961 March 3 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Antares.
  • Re-entry Vehicle test - . Nation: France. Agency: ONERA. Apogee: 150 km (90 mi).

1961 March 6 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Antares.
  • Re-entry Vehicle test - . Nation: France. Agency: ONERA. Apogee: 150 km (90 mi).

1961 March 7 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Antares.
  • Re-entry Vehicle test - . Nation: France. Agency: ONERA. Apogee: 150 km (90 mi).

1961 May 13 - . Launch Site: Hammaguira. Launch Vehicle: Antares.
  • Ionosphere mission? - . Nation: France. Agency: ONERA. Apogee: 280 km (170 mi).


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