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Vesta

Launch vehicle · France

Original archive entry. The text, images and links below are kept as they were written.

French LRBA Nitric acid/Turpentine sounding rocket. In the late 1950's LRBA studied several possible configurations for a 'Super Veronique' sounding rocket, with engines of 80 to 250 kN to carry a payload of 100 kg up to 600 km altitude. In 1962 CNES ordered the Vesta configuration. Static tests in 1964 led to a modest series of launches in 1965-1969.

Payload: 500 kg (1,100 lb) to a 400 km altitude. Boost Propulsion: Nitric acid/turpentine.

Subtopics

  • Vesta-1 Nitric acid/Turpentine rocket stage. 140.00 kN (31,473 lbf) thrust. Mass 5,000 kg (11,023 lb).
Country
France
Stages
Vesta-1
Agency
LRBA

Chronology

5 events

1965 October 15

Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. Launch Vehicle: Vesta.
  • FU-123 test - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi).

1965 October 25

Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. Launch Vehicle: Vesta.
  • FU-123 test - . Nation: France. Agency: CNES. Apogee: 105 km (65 mi).

1967 March 7

09:42 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. Launch Vehicle: Vesta.
  • FU-147 Biological mission - . Nation: France. Agency: CNES. Apogee: 243 km (150 mi).

1967 March 13

09:30 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. Launch Vehicle: Vesta.
  • FU-147 Biological (Macaca) Biological mission - . Nation: France. Agency: CNES. Apogee: 234 km (145 mi).

1969 November 8

Launch Site: Kourou. Launch Complex: Kourou ALFS. Launch Vehicle: Vesta.
  • FU-189 Star pt test - . Nation: France. Agency: CNES. Apogee: 204 km (126 mi).