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
Lex
French sounding rocket. Single stage vehicle.

Status: Retired 1967. First Launch: 1964-04-25. Last Launch: 1967-11-01. Number: 8 . Thrust: 10.00 kN (2,248 lbf). Gross mass: 100 kg (220 lb). Height: 3.40 m (11.10 ft). Diameter: 0.16 m (0.52 ft). Apogee: 130 km (80 mi).

Subtopics
MT 27 SNECMA solid rocket engine. Lex first stage.
Country: France. Launch Sites: Ile du Levant. Stages: MT 27. Agency: ONERA, SNECMA. Bibliography: 2.
1964 April 25 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex. FAILURE: Failure.
1965 June 1 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex.
1965 June 1 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex.
1965 June 1 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex.
1967 November 1 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex.
1967 November 1 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex.
1967 November 1 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex.
1967 November 1 - . Launch Site: Ile du Levant. Launch Pad: CERES. Launch Vehicle: Lex.
Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use