Series of Thiokol solid rocket engines used on the Scout launch vehicle.
First Launch: 1960年11月25日. Last Launch: 1961年05月13日. Number: 6 .
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).