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According to what is wrote in page 26 of Fana 461 (my English is not as good to be sure. It's why I give the French version before, for better translators) :"Le TF 306 se présentait comme un bon compromis jusqu'à mach 2.5, où son rendement diminuait. SNECMA proposa plusieurs moteurs combinant turboréacteur et statoréacteur à partir du TF 306"I understand"TF 306 engine was a good compromise to Mach 2.5, where its performances were declining. From the TF 306, SNECMA proposed several engines combining turbojet and ramjet."To finish with the engines, Fana 461 + French SP 1 give :-SNECMA TF 306 DS : 11 800 - 12 000 kgp-SNECMA M51-30 : 12 500 kgp-SNECMA M51-45 : 7 500 kgp-SNECMA M51-53 : 13 000 kgp
According to what is wrote in page 26 of Fana 461 (my English is not as good to be sure. It's why I give the French version before, for better translators) :
"Le TF 306 se présentait comme un bon compromis jusqu'à mach 2.5, où son rendement diminuait. SNECMA proposa plusieurs moteurs combinant turboréacteur et statoréacteur à partir du TF 306"
I understand
"TF 306 engine was a good compromise to Mach 2.5, where its performances were declining. From the TF 306, SNECMA proposed several engines combining turbojet and ramjet."
To finish with the engines, Fana 461 + French SP 1 give :
-SNECMA TF 306 DS : 11 800 - 12 000 kgp
-SNECMA M51-30 : 12 500 kgp
-SNECMA M51-45 : 7 500 kgp
-SNECMA M51-53 : 13 000 kgp