I just plain disagree with all the anti B-70 posts. Look logically at a couple of facts. The SR-71 was NEVER shot down by missles, even tho fired at several thousand times. SAMs are short range, and the B-70 would run them out of fuel before they could get to the B-70. Also we are still flying the B-52 as a viable weapon system. So tell me if the AF thinks a B-52 flying at 45,000 feet and 600 mph, why wouldnt a B-70 flying at 80,000 feet and mach 3 be more surviable? Remember these days a B-52 does not fly directly over the target, they stand off and fire weapons at the target hundreds of miles away. A B-70 would do the same thing except higher and faster and closer, and still be able to get away.
I contend that an enemy would have to fill their country with SAM sites every 10 miles all over the country to be able to shoot down a B-70. So many sites that a country would go broke doing so.
Lastly a MIG-25 was mentioned, as the USSR response to the B-70. When one was handed over to us in Japan, it was found out that it was so poor quality there was a placard on the panel that said “dont exceed mach 2.8”. Also its maneuverablity was in question. So how was a plane that was much slower and less maneuverable going to shoot down the B-70?
It remains that IMO NcNamara and his “whiz kids” that gave us the Edsel were idiots!!!!!!
With all due respect, things are not as simple as a game of Trump cards, with top speed trumping another.
You’re having an extremely simplistic look at things, and ignoring things, many of them already mentioned here, that don’t suit your narrative.
The enemy won’t just conveniently cancel all their SAMs and interceptors that are in development or entering service.
A video tape I have on the testing of the B-70 said at low altitudes, ground hugging, the aircraft handled very well.
It might have made a good low altitude strike aircraft that could boogie at extreme speeds for egress purposes.
Going low altitude would have nullified every single possible advantage the B-70 possibly had.
Going at any sort of worthwhile speed for prolonged amounts of time near the deck in that aircraft, with its wing area of almost 600 square meters, would probably have shaken the crews eyeballs out of their sockets, apart from the fact that the aircraft themselves would have been only fit for scrap after a few years.
HPTs are apparently complete for stage-2 engine.
http://www.militarynews.ru/excl.asp?ex=171
Ran this through a translation programme.
Engine for aircraft of the fifth generation will be different from the previous generation increased engine specific thrust, less weight, a lower specific fuel consumption and the availability of new solutions for low visibility.
In aviation engine everything is important. One of the most difficult parts of the engine is a high pressure turbine. We were asked to make a turbine running at this level of temperature, under which metallic nickel alloys just melt. This work was successful.
The heart of the aviation engine high pressure compressor is. The level of his goodness direct are all essential characteristics of the engine. The amount of detail in the new compressor high pressure, we were able to cut almost by half compared to the previous phase of the compressor, it provided a significant increase in work by one step. The cost of producing such a compressor will not exceed the cost of manufacturing the engine BUILDUP of the fourth generation. And it is subject to the application of new materials and technologies.
The “Saturn” has experience and good results using new materials developed by the all-Russian Scientific Research Institute of aviation materials (VIAM).
First of all, it is, of course, vane motors are heat resistant nickel alloys. Turbine blade is an absolutely unique product. It is a complex spatial structure, which should work at temperatures above 2000 k.
There are also proprietary materials “Saturn”. We are ready to offer them a new generation engine. These materials allow one and a half times increase engine life for the same temperatures.
Today there is a lot of talk on the application of composite materials. In the new engine for the PAK FA are composites that are built not only on the cold part of the polymer matrix, as well as details on the high temperature created compositions. The work of the NPO “Saturn” is already quite long.
Today in “Saturn” is serious research on the development of fifth-generation engine technology, which is called “variable cycle” engine. Studies that show that a certain transformation Thermodynamics of the engine due to design changes, you can significantly improve the performance of the engine for subsonic and supersonic flight regimes. One such transformation can be the use of the third circuit. All of it is provided.
Now I understand that true meanings can get “lost in translation”, but I found some of this very, very interesting.
Each SAM site could fire more than one missile.
There were more than one SAM site.
As can be seen just a little later from the S-75 (SA-2) deployment during the Cuban Missile Crisis, where another U2 was shot down, killing Major R Anderson.
There were, as mentioned, developed versions in the pipeline, as well as other long range, high altitude SAMs in development.
Which would have been in time for the B-70, which first flew in prototype form toward the end of 1964.
Even allowing for the slowdown of that programme, it is doubtful it would have been in service earlier than the late 60’s.
It is worth noting that the B-70 operational profile, from which its design followed, was from before the time that the USSR fielded SAMs.
IMHO, of course.
What about SAM sites downrange of the radar?
What about multiple SAM sites, as the Soviets did indeed employ?
The Soviets fired 3 SAMs actually, not a salvo of many SAMs.
It was one of the early variants of the S-75 (SA-2), which had also shot down a Taiwanese Canberra at 20 000m the year before.
The Soviets were obviously known to be working on developed variants of the S-75, which did enter service, and also other long ranged high altitude SAMs to complement it in service.
Not that I wouldn’t have loved to see the B-70 in service.
And I agree that it would likely have helped out on other projects.
The Nesher and Kfir were produced with French assistance.
I made a long post on another thread regarding this.
A brief reflection on the timeframe and industrial capability at the time is all you need.
This is why I rarely bother to visit AFm forums.
Almost no mods, and the same old usual suspect, Scooter, who will derail threads in a manic attempt to bring the F-35 into every single thread.
Moderators…where are you?
That article is long since discredited, due to the obvious gross errors in it.
No reason not to include other AAMs like IRIS T, ASRAAM, Python 5, A darter, AAM-5, PL-10.
Indeed.
Public domain information shows the A-Darter to have a 180 degree look angle, 120 degree per second track rate, LOAL and LOBL, thermal imaging, laser proximity fuse, and thrust vecoring control allowing up to 100g’s peak.
The Umkhonto SAM’s birth lies in the SAHV-3 SAM from the 1990’s.
The Block 1 missile has now been replaced with the Block 2, which has a range of 15km and a ceiling of 10 000m.
The Umkhonto ER missile that is now in testing has a range of 20km and higher ceiling, and is dimensionally identical to the current Block 2, and will be retrofitted into it’s place.
The Umkhonto R is the radar version that work has been done on, and this is heavier and longer, with a range of 25km and a ceiling of 12 000m.
In the pipeline are versions stretching the range out to 30km, as well as a radar version taking range out to 80km.
Denels new Marlin BVRAAM and R Umkhonto will share seeker technologies.
The Umkhonto is currently operated by South Africa and Finland, and it has been reported that Algeria will fit it onto the new Meko A200 class that are under construction.
Marcel Dassaults incomparably beautiful and long lived Mirage III, nose radar versions.
The other thing is that until one has experienced the crucible of combat, all analysis is academic and hypothetical.
As I keep saying last time China went to war in any fashion was unsatisfactory 1979 invasion of Vietnam.
The modern PLA has not encountered war even in the limited fashion that the US and co and Russia have over the last 20 years.
I’ll ask again:
Why do you keep bringing up a conflict from almost 40 years ago in this thread of yours about the modern Chinese military?
That’s like bringing up WW2 in the 1980’s.
You may as well bring up the US performance in Vietnam from the same era.
Like the modern US forces, comparing the modern Chinese forces to a conflict from almost 40 years ago makes absolutely no sense.
Yet you couldn’t repeat your performance against Vietnam.
Interesting
Not nearly as interesting as your reasons for starting this thread, and your contradiction about the modern Chinese military whilst using a conflict that happened in the 1970’s as an “example”…
Mirage F-1 also called Mirage IIIF.
That is the first I’ve ever heard that.
Are you sure?
I think it is perhaps a stretch to call the Mirage III and Mig 23 contemporaries.
Operational dates:
Mirage III – 1961
Mirage IIIE – 1964
Mirage 5 – 1967
Mig 23 – 1970
Mig 23MS – 1973
The Mig 23MS was only operational from 1974 in the Middle East.
That’s basically a decades difference, in a time when aviation was forging ahead in leaps and bounds rapidly.
The Mirage is far closer in date and is far more analogous with the Mig-21.
The fact that the Mirage III platform is still gainfully employed almost 60 years from it’s introduction (including in vastly reworked, rebuilt, and updated form) speaks volumes about how Marcel Dassault got that design neatly balanced and just right.