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| View Poll Results: Which is the better bomber? | |||
| Tu-95 |
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8 | 22.22% |
| B-52 |
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24 | 66.67% |
| Neither |
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4 | 11.11% |
| Voters: 36. You may not vote on this poll | |||
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#16 (permalink) | |
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Contrary by nature.
Military Professional
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#17 (permalink) | |
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Contributor
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The fact that the B-52 has undertaken loads more missions and dropped loads more bombs only serves to verify the capability of the B-52, and not degrade the capability of the Tu-95. |
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#18 (permalink) | |
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Resident Curmudgeon
Military Professional
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A closer me vs you machup would pit the TU-95 against the P-3 |
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#19 (permalink) | |
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Military Professional
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Semper in excretum. Solum profunda variat. |
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#20 (permalink) | |||
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Contrary by nature.
Military Professional
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Bear D- cruising speed 442mph 6-10 missiles Kh-55 1000lb warhead 1864 miles B-52H cruising speed 552 (+110mph) 20 tomahawks each with 1000lb warhead and 1553 mile range (+10/14 missiles) B-52 more punch more targets Bear-D greater stand off range |
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#21 (permalink) |
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Field mechanik
Senior Contributor
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true, but for the price of 1 b 52 you get more than 1 bear, and if you lose 1 out of 1, bad, 1 out of 3(for examlpe) not so bad.
you did mention tu is a different purpose bomber, you are 100% correct, than this vs thread is as valid as pitbull vs spaniel. lets compare stratigic bomober to the same class bomber, which would be, either backfire, or tu 160.
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"Democracy is two wolves and a lamb voting on what to have for lunch. Liberty is a well-armed lamb contesting the vote!" B. Franklin |
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#22 (permalink) |
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Senior Contributor
Join Date: 01-27-06
Location: DPRK, Democratik People's Republik of Kalifornia
Posts: 9,381
Country:
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I did...sort of. The 8 propellers on the 4 turbine engines are so big and spin so fast, their tips break the sound barrier to generate mini sonic booms. Or so I've heard. Most Bear crewmen suffer from hearing damage. Is that true?
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"Only Nixon can go to China." -- Old Vulcan proverb. |
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#23 (permalink) |
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Military Professional
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Truthful answer is; I don't know, but I tend to doubt it as if the tips of the props were supersonic there would be a great loss in propulsive efficiency due to the shock waves (and thus turbulence) generated. This could also cause sonic fatigue on the rest of the airframe.
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#25 (permalink) | |
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Distant Deeps or Skies
Senior Contributor
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http://www.aviapedia.com/files/bombe...95/Tu-95MS.jpg The cross-sectional area is gigantic so that they won't have to spin so fast to generate the same displacement.
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HD Ready? |
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#26 (permalink) | ||
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Contrary by nature.
Military Professional
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The best head to head is Tu-160 vs the B-1b The lancer is slower, shorter legged (w/o a2a refueling), smaller and has a smaller payload but more airframes better avionics, more flight time and much better RDS reduction. Either craft is a fear of god weapon against any other nation on Earth. |
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#29 (permalink) | |
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Contributor
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Quote:
C:\ZIP\NEWHOME\NWS001\combair008.htm |
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#30 (permalink) |
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Contributor
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Glyn is right I reckon, many underestimate the Bear...at their peril!
It has embarrassed a few maritime patrol aircraft like the Nimrod a few times! It has also demonstrated a remarkable climb rate and acceleration to embarrass a few fighters, although briefly, I am talking Tornado F.3 of course, which frequently needs one afterburner lit to keep up at altitude. More a measure of the deficiencies of the Tornado which was designed for low and fast rather than high altitude performance, but on acceleration, at least initially, the Bear has left Egg on a few NATO fighter drivers faces. The propellers TIPS actually reach transonic speeds ( Mach 0.8 to 1.2) at full chat, and it is an extremely noisy aircraft. A lot of helicopter rotor tips and even tail rotor tips reach transonic speeds but it is not desirable. Speeds of 575 kts have been quoted for the Bear. For anyone familiar with fluid dynamics, reference Bermouli`s equations for compressible flows at low Mach for an understanding of air flows and propeller behaviour.
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"Liberty is a thing beyond all price. Last edited by Tin Man : 04-01-2008 at 18:12 PM. Reason: Added note.. |
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