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Emma
French test vehicle. Two stage vehicle consisting of 1 x Emma Booster + 1 x Emma

Status: Retired 1963. First Launch: 1963-02-19. Last Launch: 1963-10-10. Number: 8 . Height: 3.90 m (12.70 ft). Diameter: 0.14 m (0.45 ft). Apogee: 69 km (42 mi).



Subtopics

SEPR P163 Matra solid rocket engine. Emma first stage.

SEPR P191 Matra solid rocket engine.

Family: test vehicle. Country: France. Launch Sites: Hammaguira. Stages: SEPR P163, SEPR P191. Bibliography: 2.

1963 February 19 - . Launch Site: Hammaguira. Launch Vehicle: Emma.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 60 km (37 mi).

1963 February 20 - . Launch Site: Hammaguira. Launch Vehicle: Emma.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 60 km (37 mi).

1963 February 26 - . Launch Site: Hammaguira. Launch Vehicle: Emma.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 32 km (19 mi).

1963 February 28 - . Launch Site: Hammaguira. Launch Vehicle: Emma.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 55 km (34 mi).

1963 May 10 - . Launch Site: Hammaguira. Launch Vehicle: Emma.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 25 km (15 mi).

1963 May 10 - . Launch Site: Hammaguira. Launch Vehicle: Emma.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 18 km (11 mi).

1963 October 8 - . Launch Site: Hammaguira. Launch Vehicle: Emma. FAILURE: Failure.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 2.00 km (1.20 mi).

1963 October 10 - . Launch Site: Hammaguira. Launch Vehicle: Emma.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 55 km (34 mi).


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