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| Post-War A place to discuss post WWII to Vietnam. |
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| | #136 | |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,881
| Quote:
__________________ > I Support Doug Gillis < | |
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| | #137 |
| aka Dickcheese ![]() Join Date: Apr 2005 Location: Washington State
Posts: 14,012
| Well said Instal. Welcome to the forum.
__________________ "Some people spend an entire lifetime wondering if they made a difference in the world. But, the [U.S.] Marines don't have that problem." -- Ronald Reagan Master of Duplicate Posts |
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| | #138 |
| Junior Member Join Date: Oct 2007
Posts: 4
| Arrow Reference Material Ok, the latest Arrow literature, 1) "Avro Aircraft and Cold War Aviation" by Randall Whitcomb. This book was called the definitive Avro book by Jim Floyd vp Avro Canada (Engineering) and the only book that Jim has ever endorsed. 2)"Storms of Controversy" by Palmiro Campagna. DND scientist and engineer that studied the Arrow for over 30 years. 3) "Requiem for a Giant" Campagna's latest book contains the latest information derived from the latest documents to be declassified. This is where I found the Jetliner info that I mentioned in a earlier post. The history of the Arrow changed when the latest files were declassified, infact so, it made any book published even 7 years ago out of date, and in error. Allong with the published government dogma. Palmiro was kind enought to host our "Ask the Expert" pages on the website they are here; ATE1 There are many many Arrow books some good some very bad, read them all with an open mind. We also have some secret documents, the "Shaw Report" that was written at the time of the closure. We compiled the 74 page report onto a "Interactive CD" that we use for fundraising, has pictures and a lot of stuff. That's here; Avro Arrow Online Store-MULTIMEDIA If your interested. I think Palmiro said it perfectly : The Arrow is still being debated because it affected so many people and impacted all our lives over the last 40 years. It is being debated because of the way the decision was taken, with little or no explanation to Canadians. It is being debated because of all the rumors that sprang up about poor engineering, political interference, soviet moles etc. It is still being debated because there remains more truth to be told. It is still being debated because those who were maligned unnecessarily over the years will not forget. It is still being debated because the historians have only partially admitted they have been wrong over all these years. (Some of them finally conceded the Arrow was technically superior but they still erroneously claim it was costing too much.) There are many more reasons than this. I hope you all enjoy the Arrow talk, I think it's great, even the bad stuff LOL. Cheers and Best Regards Scott McArthur Research/Technical Director Arrow Recovery Canada Inc. Oh yes, for the Jetliner fans, Jim Floyds "Avro Canada C102 Jetliner" book has some Arrow info. It's been out of print for many years. I found mine on Ebay and was lucky enough to have Jim sign it! PER ARDUE AD ASTRA |
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| | #139 | |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,881
| Quote:
PS - I'll be in Toronto tomorrow night - LOL!!!
__________________ > I Support Doug Gillis < | |
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| | #140 |
| Member Join Date: Oct 2007 Location: Victoria BC
Posts: 97
| One last note about the Arrow. There is one that survived and it is flown by Elvis but he flew into the Bermuda triangle and neither have been seen again.
__________________ "An appeaser is one who feeds a crocodile hoping it will eat him last" Winston Churchill |
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| | #141 |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,881
| Oh I don't know - I heard it was seen on the runway at Area 51!!!
__________________ > I Support Doug Gillis < |
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| | #142 |
| Senior Member | "20) First missile armed a/c to have a combat weight thrust to weight ratio approaching 1 to 1. Few have been able to copy that." The F-104 had between a .56 to a .75 depending how much fuel it carried and how it was armed. The Arrow had a Thrust/weight: Dry: 0.439 With afterburner: 0.650 - it also had two engines... The F-4 had a thrust to weight ration of .86! I don't know the exact thrust:weight ratio of a Lightning - but I do know that at one point during its flight it reached 1:1 when fuel had been burnt off. At that time it should get back to base pretty sharpish - but still. And I don't if the P.1B was the first to supercruise in the world, but it's pretty damn close to the first.
__________________ "When you go home tomorrow, don't expect anyone to know what you have been through. Even if they did know, most people probably wouldn't care anyway. Some of you may get the medals you deserve, many more of you will not. But remember this, all of you are now members of the front-line club, and that is the most exclusive club in the world." - Lt. Col. Matthew Maer CO 1st Battalion, the Princess of Wale's Royal Regiment. Camp Abu Naji, Oct. 2004 |
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| | #143 |
| aka Dickcheese ![]() Join Date: Apr 2005 Location: Washington State
Posts: 14,012
| What?? Really?? Almost 1:1? That defies physics for this airframe. Specifications (Arrow Mk 1) Data from The Great Book of Fighters[21] General characteristics Crew: 2 Length: 77 ft 9 in (23.71 m) Wingspan: 50 ft 0 in (15.24 m) Height: 20 ft 6 in (6.25 m) Wing area: 1,225 ft² (113.8 m²) Airfoil: NACA 0003.5 mod root, NACA 0003.8 tip Empty weight: 49,040 lb (22,245 kg) Loaded weight: 56,920 lb (25,820 kg) Max takeoff weight: 68,605 lb (31,120 kg) Powerplant: 2× Pratt & Whitney J75-P-3 turbojets Dry thrust: 12,500 lbf (55.6 kN) each Thrust with afterburner: 23,500 lbf (104.53 kN) each Performance Maximum speed: Mach 2 (1,307 mph, 2,104 km/h) at 50,000 ft (15,000 m) Cruise speed: Mach 0.91 (607 mph, 977 km/h) at 36,000 ft (11,000 m) Range: 360 NM (410 mi, 660 km) Service ceiling: 53,000 ft (16,150 m) Wing loading: 46.5 lb/ft² (226.9 kg/m²) Thrust/weight: Dry: 0.439 With afterburner: 0.650 Even if you don't trust the T/W ratio quoted, just do the math. T/W (empty)= 0.96 T/W (loaded) = 0.82 [I assume loaded means max internal fuel/no weapon loadout] T/W (MToW) = 0.68
__________________ "Some people spend an entire lifetime wondering if they made a difference in the world. But, the [U.S.] Marines don't have that problem." -- Ronald Reagan Master of Duplicate Posts |
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| | #144 |
| Senior Member Join Date: Apr 2005 Location: niagara falls
Posts: 5,964
| What he is referring to is the next one off the production line that was powered by 2 of the indiginous Orenda Iroquois with 20000,lbs thrust tests up to 30000lbs in burner mode. It was was test flown on the B47 they were able to shut down all the 47 engines and fly it solely with the Iroquis it supposedly bent the 47. The engine is visible on the aft starboard Last edited by pbfoot; 10-21-2007 at 10:48 AM. |
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| | #145 |
| aka Dickcheese ![]() Join Date: Apr 2005 Location: Washington State
Posts: 14,012
| I don't know anything about this experimental engine, but suspect that the hot section lifespan was SEVERELY limited due to the metallurgy of the day. And most likely of such grave limitations as to not be of production quality. Zoom fast. Throw it away.
__________________ "Some people spend an entire lifetime wondering if they made a difference in the world. But, the [U.S.] Marines don't have that problem." -- Ronald Reagan Master of Duplicate Posts |
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| | #146 |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,881
| There is no doubt the Arrow "would of" been a lot hotter with the Orenda Iroquois, but again we're looking at a "would of should of." As Matt pointed out I think there might of been some engine life limitations and again the fuel consumption of this beast was also something to consider.
__________________ > I Support Doug Gillis < |
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| | #147 |
| Senior Member Join Date: Apr 2005 Location: niagara falls
Posts: 5,964
| I don't have the knowledge of metals and stress and fatique to talk about this on your level but maybe this link I'll provide can clear up any of the questions or doubts you or I might have as it tells what is what in retrospect to the metals. But it did complete 5000hrs of ground running |
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| | #148 |
| Member Join Date: Oct 2007 Location: Victoria BC
Posts: 97
| Those of us that are passionate about the Arrow have been accused of stating how good it is without facts. Is this statement not going out of your way to say that it is a bad performer without facts?
__________________ "An appeaser is one who feeds a crocodile hoping it will eat him last" Winston Churchill |
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| | #149 |
| IP/Mech THE GREAT GAZOO ![]() Join Date: Apr 2005 Location: Colorado, USA
Posts: 16,881
| You are correct and the only thing I could say about that is the across the board hot section and TBO increase seen on military turbine engines of the period as the continued into service. I know there are dozens of J-79 TCTOs that replaced many internal parts, bearings etc that increased engine life, I would think the Iroquois would of fell into the same situation.
__________________ > I Support Doug Gillis < |
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| | #150 |
| aka Dickcheese ![]() Join Date: Apr 2005 Location: Washington State
Posts: 14,012
| It is a statement of fact for the technology of the day. One must assume that engines of Canadian design were no different then the rest of the world's technical prowess. Don't take it personally.
__________________ "Some people spend an entire lifetime wondering if they made a difference in the world. But, the [U.S.] Marines don't have that problem." -- Ronald Reagan Master of Duplicate Posts |
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