The first M88-3 was ground tested on 17th february this year. Snecma: 10, allée du Brévent - CE1420 Courcouronnes - 91019 Evry Cedex - France Tel. As I recollect, the fan diameter, and overall length were slightly great than for the M88-2. What precisely were the specs on the M88-3?

- Edited 1st January 1970 at 01:00, By: Scorpion82 - BillCJ 15:50, 4 April 2009 (UTC) Uncited Content. By: Scorpion82 and nw that eurostuff is 12t whale, all estimations about "exceptional abilities" gones far! A Further Step in the Modeling of the Flow in Turbine Compressors, ZéBuLoN, Numerical Microscope for Composites. - 30th November 2005 at 14:51 Permalink By: Anonymous Length 3.6 m 12-ft - Edited 1st January 1970 at 01:00. 8 More realistic virtual engines Modeling what happens in the combustion chamber as accurately as possible is very important in the design of more environmentally friendly aircraft engines ... Annular combustion chamber of an aircraft engine. By: Stealth Spy - Edited 1st January 1970 at 01:00. After the Rafale's defeat by the F-15 in Singapore, I thought it was time to ask about the status of the M88-3 program. - 30th December 2005 at 16:40 Permalink For example M88-3, CFT or AESA RBE-2. They were two versions - Edited 1st January 1970 at 01:00. Airflow 72Kg/s. As long as the RAfale weight do not increase, the RAfale customer (read France) wouldn't pay for a more powerful M88 but in a specific program funded by the DGA. I know the bulk of the article is uncited, and needs to be corrected, but I don't think … F2/F3 with options which the customer can choose. - 30th December 2005 at 14:36 Permalink By: Scorpion82 they acheived that, as benchmark proved! Snecma High Thrust Cryogenic Engines for the Next 20 Years. - Edited 1st January 1970 at 01:00. But it seems there are few informations about it in this moment. By: TinWing ODAS 2017 in Aussois, a successful event! By: TinWing Max Weight 897 kg 1,978-lb By: Scorpion82 Developement will probably be finished and the engine offered for exdport customers. Rafale Mk.2 is dead. It is said that the -3 need different air intakes on the rafale which are already fully develloped and "increase the RCS". - Edited 1st January 1970 at 01:00. - 29th November 2005 at 14:39. The "mk2" really looks like a marketing trick. - 30th December 2005 at 12:46 Permalink I know, not going to happen with both sides having good reasons not to do it, but the EJ200 is a mighty fine engine. M88-2E4: Advanced New Generation Engine for Rafale Multirole Fighter. If I follow that logic M88 is also much more advanced than the F119 of the F/A-22A. By: glitter … China Has the World's Largest Navy - What Now for the US?

- 30th December 2005 at 13:57 Permalink - 30th December 2005 at 18:04 Permalink I have always assumed that the M88-3 designation was originally meant for a higher powered M88 development, not a longer life/lower maintainence version of the M88-2? The Rafale will require larger engine intakes for the M88-3, but new intakes can be retrofitted to older aircraft with little difficulty. 9 … Oddly enough, the M88-3 was very nearly the same size and output as the EJ200. - 30th December 2005 at 17:52 Permalink Lasting 1 hour and 30 minutes, the flight was a total success, and was used to expand the flight envelope. At the moment both M88-3 and Rafale "Mk2" are deferred indefinitely. They call it the M88 ECO. But fuel consumption should be equal. It seems to me that mass flow increase from the M88-2 to the M88-3 is only half as great as the mass flow increase of the GE F414 over the original F404. - Edited 1st January 1970 at 01:00. Similarly, I haven't seen any media references to the M88-3 for quite a while? 3.) - 29th November 2005 at 16:08 Permalink

As far as the M88-3 designation being used for two variants, that's very possible. 2.) That is what was edited in the snecma website - Edited 22nd October 2019 at 22:29. By: datafuser - 29th November 2005 at 15:22 Permalink - Edited 1st January 1970 at 01:00 After the Rafale's defeat by the F-15 in Singapore, I thought it was time to ask about the status of the M88-3 program. By: NungesserC By: OPIT st. "M88-3" prototype back in the 1990s.

Did you realize we are talking here about the M88-3? The M88 jet engine built by Snecma (Safran), powerplant of the Dassault Aviation Rafale multirole fighter, has largely proven its maturity and operational capabilities, especially during the Harmattan operation in Libya, lasting eight months in 2011.

By: glitter 5.) By: datafuser The only similarity is the size and that was required due to the fact that the first two prototypes were initially powered by RB-199-34R MK104D turbofans. - Edited 1st January 1970 at 01:00. : 33 (0)1 69 87 09 00 - Fax: 33 (0)1 69 87 09 02 www.snecma.com The M88-2 engine, designed for the multirole combat aircraft Rafale, is the first in a family of new-generation engines designed to power the combat and advanced training aircraft of the 21st century. SNECMA is working on an uprated M88-3, which would have 90 kN (9,175 kgp / 20,233 lbf) afterburning thrust. I remember the M88-3 being closer to 4.0 m in length - just about the same as the EJ-200? More Job Cuts At Boeing As Profit Slumps On 737 MAX, COVID Crises, Russia Says Latest Test-Firing of New ABM Interceptor Missile Successful, EU to Allow Britain, US to Join Future PESCO Defence Projects: Report, China MoD Talking to Pentagon to “Cool Down Tensions”: Statement, Royal Navy’s Final Batch 2 OPV Sails to Her New Home Port, Sikorsky to Build Six More CH-53K Heavy Lift Helicopters, Another Littoral Combat Ship Breaks Down During Deployment, Turkish Firms Unveil ULAQ Armed Unmanned Surface Vehicle, USAF Contracts Study to Transform Airlifters in Weapon Platforms, U.S.

For the moment, however, there's been no strong user demand for the new engine; the only expected improvement is a modest update to the M88-2 to the "M88-4E" … So the Mk2 is dead, but not the Rafale with the same capabilties. By: TinWing

I'm not sure how well the EJ-200 could sustain when flying at low altitude. By: Petros - Edited 1st January 1970 at 01:00.

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Semi-Lobster 15:46, 4 April 2009 (UTC) Becuase the company now calls itself "Snecma", and the engine the "Snecma M88". The SNECMA M53 is an afterburning turbofan engine developed for the Dassault Mirage 2000 fighter by Snecma. - 30th November 2005 at 19:19 Permalink COURCOURONNES, France: The first test flight of a Rafale fighter powered by the Snecma (Safran group) M88-4E engine (formerly designated the “TCO Pack”, for total cost of ownership) took place on March 22 at the Istres air base in southern France. All other SNECMA engine articles have the acronym capitalised, why not this article? - Edited 1st January 1970 at 01:00. - Edited 1st January 1970 at 01:00. - 30th December 2005 at 18:21 Permalink Is the M88-3 dead, along with any chance of an upgrade Rafale "Mk2?". But if there will be an export customer which requires the M88-3 it will be ready in the not to distant future. - 30th December 2005 at 04:26 Permalink 1.) to achieve this. You must know it :rolleyes: . - 30th December 2005 at 18:08 Permalink Shouldn't this article be 'SNECMA M88' instead of Snecma M88? http://antislashe.free.fr/. Max Weight 985 kg 2,172-lb In fact EJ200 has nothing to do with RB-199.