I miss the pictures!
Mig-21 in Laos 2014. Xieng Khouang (XKH) Airport, Phonsavan
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Did Google Earth Just Unveil Lockheed’s Mysterious Mach-6 Spy Plane? (PHOTO) post #4528
This object is presumably a RCS test article because itˋs on an RCS test range, not on an airfield.
F-35B? Isn’t that a F-35A?
There are three main reasons why there has been a requirement in the past for a two seater.
1. Trainer
2. Information Management
3. Situational Awareness1. Trainer – 5th gen fighters to date have been easier to fly than their predecessors so type-specific airborne training has not been needed.
2. Information management (aka RIO) – In the days of Federated sensors that fed raw data to the crew, a RIO was needed to sift through the data, compare information, and manage the systems. Modern computers can do that automatically now.
3. Situational Awareness – In previous generations it was difficult for the on-board systems to determine what was around the fighter, both in the air and on the ground. It required a 2nd crewman to help build a picture of the battlefield and present it to the crew. Modern systems like FLIR, HMDS, EODAS, datalinks, etc allow that information to be gathered, classified, and presented tot he pilot without the need to manually process it.
Sorry, but I think you forgot the main reason:
– costs
The pilot was injured and brought to a hospital in Besancon, which he could leave yesterday to come back to Switzerland.
Flying at 20 degrees
In AIR International July 2015 I read in there F-22 Raptor supplement on page 55:
“It can cruise at 40’000ft at Mach 1,2 with the nose heading 20 degrees off the course of travel …”
This is difficult to understand for me. What do you think about that?
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All those who’s memory reaches far back …
… might realise the SR-72 is not as new as it seems.
Aerojet has shown this aircraft (see picture 1 below) as the TriJet concept (Link here)
in the summer of 2011. The main difference to the SR-72 is the engine, which then consisted of three instead of two components: a turbine, an ejector ramjet and a dual-mode ramjet (see picture 2 and 3).
Perhaps this is the reason why the engine nacelles seem so huge!
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Would be delighted to see the source of that image. Thx in advance!
But first thing that come in mind is the lack of the Rocket accelerator and the 3D layout of the engines arrangement.
Last but not least, it’s a SCramjet
Picture is from Aviation Week, here
SR-72 Engine Layout
Looking at the layout of the TBCCE, I got a question to all of you: Why this relatively big distance between the Turbine and the Ramjet?
I think the original article by Sweetman mentioned of a technology for integrating Turbofan+Scramjet in the same engine.
Sweetman, at least in his book, supossed a RBCCE (ROCKET based combined cycle engine) not TBCC like in this SR-72 project
I used the search engine and F-313 Qaher gave nothing.
Thats because it was called “Quaher 313” there instead of “F-313 Qaher”. A search for “Qaher” only delivers correct results.
Ok, the use of a search machine can be a bit tricky sometimes…
This has been discussed weeks befor in this forum, see here:
please use the search engine before open a new thread of an old topic!
…
As for the auxiliary intakes, try to guess why the wire grilles on the F-117 were sized the way they were ;).
In those good old days, the saying was going the size of the “wire” grilles had something to to with the wavelength of the radars trying to get the F-177A.