Daniel (rocket)

From Wikipedia, the free encyclopedia
Daniel
Country of originFrance
Date1959
DesignerKorea Aerospace Research Institute
StatusRetired
experimental rocket
Daniel rocket (left) and the Onera sounding rocket family.

Daniel (OPD-220-ADX) is the designation for a French experimental rocket, a precursor to the Israeli Jericho ballistic missile.[1][2]

Description[edit]

It consisted of 3 stages (first stage: SPRAN-50, second stage: Jericho, third stage: Mélanie.[3] The Daniel reached a maximum height of 130 km and had a takeoff weight of 1000 kg, a diameter of 0.40 m and a length of 8.40 m[1]

Launches[edit]

Daniel was launched three times between 1959 and 1961 by ONERA from Centre d'Essais et de Recherches d'Engins Speciaux - Ile de Levant.[4][2]

Daniel launches[2][4]
Date Mission Apogee
1959 January 27 Atmosphere radioactivity 127 km (78 mi)
1961 October 5 Test / aeronomy mission 130 km (80 mi)
1961 October 9 Test / aeronomy mission 130 km (80 mi)

See also[edit]

References[edit]

  1. ^ a b Wade, Mark (2019). "Daniel". Encyclopedia Astronautica. Archived from the original on 2022-05-16. Retrieved 2023-11-11.
  2. ^ a b c Serra, Jean-Jacques (2007-01-13). "ONERA rockets". Rockets in Europe. Archived from the original on 2007-01-13. Retrieved 2023-11-11.
  3. ^ Christophe Rothmund (2010). History of Rocketry and Astronautics: Proceedings of the Thirty-Fifth History Symposium of the International Academy of Astronautics : Toulouse, France, 2001. American Astronautical Society. ISBN 978-0-87703-555-8.
  4. ^ a b Krebs, Gunter D. (2023). "Daniel (OPD-220-ADX)". Gunter's Space Page. Retrieved 2023-11-11.