Qualification of the basic Snecma M88-2 was completed in early 1996, with the first production engine delivered at the end of the same year. The M88-2 has a thrust-to-weight ratio of 8.5, producing 11,250/16,850lb of dry/afterburner thrust (50/75kN). The engine has proved extremely ...
M88-2发动机的认证工作于1996年完成,第一台生产发动机在同年年底交付。它采用模块化设计,方便制造和维护,并且可以使老旧发动机在可用时通过安装改进的部件进行升级,例如将现有的M88-2升级到M88-4E标准。2010年5月,一架阵风战斗机首次配备了M88-4E发动机进行飞行,这是一种升级型号,比前置的M88-2具有更大的推力和更...
¢M88……….……….……..………..…p.8 ¢TP400……….….p.9 ¢Spaceengines..………..………..p.10 ¢MROnews……..………..……….…p.11 Snecmapresscontacts: AntoinetteMenard/VincentChappard Tel.:+33(0)674781065/+33(0)662772276 antoinette.menard@snecma.fr/vincent.chappar...
Devaux C. Snecma' s M88- 2 Engine Rises to the Challenge[J]. Air & Space Europe. 1999,1 (3) : 84 - 85.Devaux C.Snecma′s M88-2 Engine Rises to theChallenge.Air and Space Europe. 1999Devaux C.Snecma′s M88-2 Engine Rises to theChallenge. Air and Space Europe . 1999...