Bummer.For some reasons i too cannot see them after posting.
Bummer.For some reasons i too cannot see them after posting.
Jetmaster was a better plane, but for sheer awesomeness of name, it just isn't even in the same league.
Hint hint guys who designed this BI-2 rocket fighter (Berezniyak.A.Ya and Isaev.A.M )is actually never ever imprisoned in Gulag. However test pilots is killed in the crash when plane reached +800km/h because it doesn't have swept wing and plane took sharp uncontrollable nosedive due weird supersonic physics that prevent non-swept wing aircrafts from reaching speed of sound.You might have added a background story. I always find the life, (and death and imprisonment and torture) of engineers in Stalin's Soviet Union fascinating.
The guys who built the fighter used plywood. The guys who made the rocket motor were purged. Korolev was a lucky one. A 5mm thick aluminum firewall was built to separate the pilot from the rocket fuel after.Hint hint guys who designed this BI-2 rocket fighter (Berezniyak.A.Ya and Isaev.A.M )is actually never ever imprisoned in Gulag. However test pilots is killed in the crash when plane reached +800km/h because it doesn't have swept wing and plane took sharp uncontrollable nosedive due weird supersonic physics that prevent non-swept wing aircrafts from reaching speed of sound.
The guys who built the fighter used plywood. The guys who made the rocket motor were purged. Korolev was a lucky one. A 5mm thick aluminum firewall was built to separate the pilot from the rocket fuel after.
The Miles M.52 and Bell X-1 both had straight wings.
Hint hint guys who designed this BI-2 rocket fighter (Berezniyak.A.Ya and Isaev.A.M )is actually never ever imprisoned in Gulag. However test pilots is killed in the crash when plane reached +800km/h because it doesn't have swept wing and plane took sharp uncontrollable nosedive due weird supersonic physics that prevent non-swept wing aircrafts from reaching speed of sound.
If you're in a rocket fuelled fighter that's on fire, I'd be more worried about the flames getting through to the fuel tanks than the cockpit. The firewall just gives you a second or three to get out before the whole thing turns into a fireball.I suppose a quarter of an inch of Aluminum is better than nothing. Though it would burn through faster than a beer can in a bonfire.
I like to know from which sources you based alternative facts of yours? Because you can't base your claims on memes. The guys who made the rocket motor were purged.
The Miles M.52 and Bell X-1 both had straight wings.
I like to know from which sources you based alternative facts of yours? Because you can't base your claims on memes
2) Huh yes after bit of digging swept wing Me 262 experienced uncontrollable nosedives at 800~900 km/h .
My alternate facts come from my feeble mind, after years ago reading the history of Korolev, and stories of the RNII, producers and researchers of rocket motors.
I don't know how the Me-262 is relevant.
Anyway jokes aside from what book you get information because it's reek like Rezun's mad ramblings and klukwa as hell .My alternate facts come from my feeble mind, after years ago reading the history of Korolev, and stories of the RNII, producers and researchers of rocket motors.
I don't know how the Me-262 is relevant.
Anyway jokes aside from what book you get information because it's reek Rezunoidism .
2)I think we have misunderstanding here .I presented argument that not entire right, you point out that i wrong 3) I conceded point and used Me262 as example of holes in my previous statement (IE: Me 262 has swept wings yet it still experienced severe sonic barrier compression issues which means problem lies somewhere else.)
Not exactly - the Me-262 wings are unswept inboard of the engines, but they need to be swept over the entire span to have a significant impact. In any case, swept wings help a bit by increasing the speed at which compressibility effects become a problem but what they don't do is eliminate the problems - they just kick them down the road a bit to what will hopefully be a high enough speed you don't have to deal with them. That's why all commercial airliners have swept wings - it reduces the effective speed over the wings for compressibility issues into the optimum range for the the aerofoil they want to use.I conceded point and used Me262 as example of holes in my previous statement (IE: Me 262 has swept wings yet it still experienced severe sonic barrier compression issues which means problem lies somewhere else.)
Uh... no. See https://history.nasa.gov/SP-468/ch10-4.htm for a good explanation - critical Mach is a function of 1/cos(sweep angle) - 35° happens to be a sweet spot for getting above the speed of sound without serious side-effects (it increases critical Mach by about 20%), but the effect is measurable for any sweep at all.The Me262's wings were swept at 18.5 degrees due to heavier engines being installed. Aerodynamic sweep to reduce the effects of compressabilty and ease transonic flight needs at least 35 degrees of sweep. Witness the Mig 15, F-86, Hawker Hunter...
Uh... no.
Yeah, that bit's correct (specifically a lack of superalloys which meant the engine was heavier than expected, from memory the problem was with the turbine which would have shifted the engine CofG aft as well). The 35° bit is aerodynamic nonsense however.Uh, I stand by what I wrote. The Me262 had its wings swept to accommodate heavier engines. Not for any aerodynamic reason.
Yeah, that bit's correct (specifically a lack of superalloys which meant the engine was heavier than expected, from memory the problem was with the turbine which would have shifted the engine CofG aft as well). The 35° bit is aerodynamic nonsense however.
Anyway jokes aside from what book you get information because it's reek like Rezun's mad ramblings and klukwa as hell .
2)I think we have misunderstanding here .I presented argument that not entire right, you point out that i wrong , I conceded point and used Me262 as example of holes in my previous statement (IE: Me 262 has swept wings yet it still experienced severe sonic barrier compression issues which means problem lies somewhere else.)