Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
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.
  • Nation: Syria. Agency: LRS. Apogee: 200 km (120 mi).

1964? - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
  • Nation: Syria. Agency: LRS. Apogee: 200 km (120 mi).

1964? - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
  • Nation: Syria. Agency: LRS. Apogee: 200 km (120 mi).

1964 September 23 - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
  • Nation: Syria. Agency: LRS. Apogee: 200 km (120 mi).

1966 May 12 - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
  • Nation: Syria. Agency: LRS. Apogee: 200 km (120 mi).

1966 August 4 - . Launch Site: Dbayeh. LV Family: Cedre 3. Launch Vehicle: Cedre 4.
  • Nation: Syria. Agency: LRS. Apogee: 200 km (120 mi).


Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use