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<blockquote data-quote="paulo" data-source="post: 943414" data-attributes="member: 5327">O último A&amp; C dá precisões sobre o M88-9 &quot; novo nome da ECO 9t&quot; fará 20.250lbf = 90.1 kN será 40kgs mais pesado que o M88 75kN e terá o mesmo custo d' utilização que o M88-4.O, gira já ao banco. as especificações são:• A/B thrust (lb) 20,250 (90.1kN)• Dry engine thrust (lb) 13,500• A/B specific fuel consumption (kg/daN.h) 1.70• Dry engine thrust specific fuelconsumption (kg/daN.h) 0.80• Air flow rate (kg/s) 72• Turbine Inlet Temperature (K) 1,850 (2,871°F)• Pressure ratio 27• Bypass ratio 0.30• Length (in) 142• Inlet diameter (in) 31• Weight (kgs) 937more efficient in consumption and cost than EJ200 &amp; F414<img src="http://img.blog.yahoo.co.kr/ybi/1/24/56/shinecommerce/folder/286/img_286_2625_5?1185020239.jpg" alt="" class="fr-fic fr-dii fr-draggable " style="" />Como dice um colega forista brasileiro...<img src="/foros/styles/default/xenforo/smilies/eek.png"&nbsp; class="smilie" loading="lazy" alt=":eek:" title="Eek!&nbsp; &nbsp; :eek:" data-shortname=":eek:" /><img src="/foros/styles/default/xenforo/smilies/eek.png"&nbsp; class="smilie" loading="lazy" alt=":eek:" title="Eek!&nbsp; &nbsp; :eek:" data-shortname=":eek:" /><img src="/foros/styles/default/xenforo/smilies/eek.png"&nbsp; class="smilie" loading="lazy" alt=":eek:" title="Eek!&nbsp; &nbsp; :eek:" data-shortname=":eek:" />Algo mas<a href="http://www.lepoint.fr/bourse/vente-du-rafale-aux-emirats-toujours-des-discussions-apres-une-crispation-cet-ete-01-10-2010-1243995_81.php">Vente du Rafale aux Emirats: toujours des discussions, après une crispation cet été, actualité Bourse : Le Point</a></blockquote>

[QUOTE="paulo, post: 943414, member: 5327"] O último A& C dá precisões sobre o[B] M88-9 " novo nome da ECO 9t" fará 20.250lbf[/B] = 90.1 kN será 40kgs mais pesado que o M88 75kN e terá o mesmo custo d' utilização que o M88-4.O, gira já ao banco. as especificações são: • A/B thrust (lb) 20,250 (90.1kN) • Dry engine thrust (lb) 13,500 • A/B specific fuel consumption (kg/daN.h) 1.70 • Dry engine thrust specific fuel consumption (kg/daN.h) 0.80 • Air flow rate (kg/s) 72 • Turbine Inlet Temperature (K) 1,850 (2,871°F) • Pressure ratio 27 • Bypass ratio 0.30 • Length (in) 142 • Inlet diameter (in) 31 • Weight (kgs) 937 [B]more efficient in consumption and cost than EJ200 & F414[/B] [IMG]http://img.blog.yahoo.co.kr/ybi/1/24/56/shinecommerce/folder/286/img_286_2625_5?1185020239.jpg[/IMG] Como dice um colega forista brasileiro... :eek::eek::eek: Algo mas [url=http://www.lepoint.fr/bourse/vente-du-rafale-aux-emirats-toujours-des-discussions-apres-une-crispation-cet-ete-01-10-2010-1243995_81.php]Vente du Rafale aux Emirats: toujours des discussions, après une crispation cet été, actualité Bourse : Le Point[/url] [/QUOTE]

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