thumb|Tibère sounding rocket scheme. thumb|Tibère (fourth rocket) as part of the Onera sounding rocket family. Tibère was a French atmospheric reentry test rocket developed by O.N.E.R.A. (''Office National d'Etudes et de Recherches Aérospatiales). It evolved from its predecessor, Bèrènice, with development initiated in 1965 to support the ELECTRE'' reentry experiment program. Tibère, standing at a height of 14.5 m and weighing 4.5 tons, operated as a three-stage rocket.
thumb|Tibère sounding rocket scheme. thumb|Tibère (fourth rocket) as part of the Onera sounding rocket family. Tibère was a French atmospheric reentry test rocket developed by O.N.E.R.A. (''Office National d'Etudes et de Recherches Aérospatiales). It evolved from its predecessor, Bèrènice, with development initiated in 1965 to support the ELECTRE reentry experiment program. Tibère, standing at a height of 14.5 m and weighing 4.5 tons, operated as a three-stage rocket.
== Description == The first stage comprised a 'SEPR-739-2 Stromboli, that, similar to Bèrènice and Titus, was encircled by four SEPR-P167 stabilization rockets. This was followed by another SEPR-739-2 Stromboli for the second stage, and the third stage housed a P.064' inherited from Diamant A.
Discovered by embedding cosine similarity (sentence-transformers MiniLM, 384-dim).