hello Erez
could not contact you by email, you must have turned this off in your profile
please change it
To MPJay
I don’t think Testor was able to do any serious research in lo properties of there F-19 plastic model as this is really not a child’s play but scientific work which needs a hole lot of knowledge and instrumentation.
BTW: even Janes, world wide known as usually good informed put the attached pic in the 1986/1987 edition of the Janes all the world aircraft. A typical example of disinformation!
sorry … here comes the pic
Mig 1.42
to SOC
“The 1.42 design featured a different intake, a different nose section, and a different wing layout.”
Could you give us a source from where you got this information? And of course, a pic would would even be more appreciated!
The Mig-37 Ferret plastic model kit was another try from Italeri to repeat the commercial succes of the F-19 model. Fantasy sells!
Well, surely not on short term! But on the long – let’s say in the next 2 decades, it could be possible. A hell of a lot of R&D has to be done first, basics, proof of concepts, cfd, scaled down models and all that stuff.
Don’t know if the USAF really needs that, but project FALCON shows, that they want more or less exactly some-thing like that (global reach from conus, hypersonic…). The question is if the government is willing and able to fi-nance it!
I meant it doesn’t make sense to use a rocket engine because you would have to carry the oxygen for the whole flight right from the start. That’s why I would prefer an airbreathing engine.
But one the other hand: a HCV must not stay inside the atmosphere for all its flight. To minimise drag and heat it could apply a skipping paten as proposed for HyperSoar (see http://www.globalsecurity.org/military/systems/aircraft/hypersoar.htm)
You mean the X-33 Venturestar?
The engine they intended to use there was a Linear Aerospike engine, pic below, for further info read
http://www.aerospaceweb.org/design/aerospike/main.shtml
As this is a rocket-engine and not airbreathing at all, it would not make sense to use it in a hypersonic cruise vehicle intended to fly in or on top of the atmosphere
I think hypersonic aerodynamics are not boring at all, particularly if you consider the thermal problem of skin friction.
But the second point you are right – propulsion is a true challenge! The X-43 shows that the development of SCRAM-engines has just begun. The only air breathing alternative I can think of is a Rocket Based Combined Cycle Engine RBCCE – whose development is not much further, as far as I know. Perhaps somebody else?
I think we recently have discussed all this in other threads before – so why shall we repeat it ?!
For the FB-22 option read:
http://forum.airforces.info/showthread.php?t=29782
The never-ending story about YF-23 and what could be done (or what already might have been done) based on this design, you find in:
http://forum.airforces.info/showthread.php?t=28409&page=1&pp=30
It all startet with an article in PopSci by Bill Sweetman, which you can still find here:
http://www.popsci.com/popsci/aviation/article/0,12543,262063-2,00.html
To Billy Bishop
The MBB Lampyriade stealth figther is a good example of first generation stealth, which is fully based on faceting the external surface of an aircraft.
To give a quick impression of the XF-108 here a pic. It’s from the higly recommended website (in french)
Twin fins – for stealth reason
As far as I remember, the twin fins came up (at least in the west…) when stealth came into play. The twin fins gave the opportunity to cant them out- or inwards at any angle.
Perhaps someone knows why Migs & Sukhois do not use this possibility?
What I still don,t know
A recommended read about SpaceShip1’s flight you find here:
http://www.aviationnow.com/avnow/news/channel_aerospacedaily_story.jsp?id=news/spa06224.xml
The remaining questions are (and I’m looking forward to
answers from some better informed members of this fo-rum) :
max. speed during descent in feathered config ?
speed to swap from feathered- to no- feathered config ?
max. speed during descent in non-feathered (landing-) config ?