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Cedre 3
Lebanese sounding rocket, developed in the 1960's by the Haigazian College Rocket Society. Cedre had three stages, was 6.8 m long, 0.52 m diameter, total mass 1250 kg, apogee capability claimed to be 180-256 km. Lower-altitude Cedre 1 and 2 rockets preceded the Cedre 3.

Status: Retired 1962. First Launch: 1962-11-21. Last Launch: 1962-11-21. Number: 1 .

Subtopics
Cedre 4 Lebanese sounding rocket, follow-on to Cedre 3, with extended first stage.
Country: xxLebanon.
1962 November 21 - . Launch Site: Dbayeh. Launch Vehicle: Cedre 3.
1964? - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
1964? - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
1964 September 23 - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
1966 May 12 - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
1966 August 4 - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
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