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Bager1968

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Viewing 15 posts - 3,181 through 3,195 (of 3,360 total)
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  • in reply to: Too Low #1336226
    Bager1968
    Participant

    All are normal for Blue Angels flight demonstrations.

    They train a lot to fly those particular profiles, and they are very good at it.

    in reply to: USAF owned Soviet Military Jet & vise versa #2587859
    Bager1968
    Participant

    >sarcasm on<
    Yes, absolutely!!

    We must never start a thread about something that has ever already been discussed… mentioned in passing… or even just thought about on this forum!!

    We only want fresh, new topics… anyone who missed out on the discussion the first time is just “Sh*t out of Luck”… and we will be insulting and rude to them if they dare break this narrowminded protocol, won’t we??
    >sarcasm off<

    Sklaucn, your thread is welcome by some of us, and we are happy to re-hash old topics with new people… after all, they just might have either a new point of view on it, or new (previously un-posted) information that we don’t!

    Keep on asking, so we all can learn and enjoy together!

    in reply to: helicopter pioneers #1251477
    Bager1968
    Participant
    in reply to: Javelin vs Sea Vixen #1251496
    Bager1968
    Participant

    There WAS a big problem with dimensions in the J79>Spey swap… the Spey’s 37.5″ diameter is for the main body (not the reheat unit), while the oft-quoted 38.3″ for the J79 is for the afterburner (reheat module) only! The diameter of the J79’s main body is only 30.3″… look at photos of both engines with their reheat units attached and you can see this clearly.

    Yes, the mass flow would be greater, requiring a redesign of the intakes, but I doubt that that would be nearly as hard as redesigning both the intakes and the entire engine area of the fuselage to fit what was actually a considerably larger diameter engine body!

    Also, the supersonic Sea Vixen would already actually be a completely different design… thinner, reshaped wing for supersonic flow… redesigned aft fuselage to take the greater stresses of a reheated Avon (or Spey)… reshaped nose and tailplane (also for supersonic flight), so redesigning the intakes would also be on the schedule, to allow for the greater mass flow of a reheated Avon as well as the changes in airflow at supersonic speeds.

    Fitting the Spey into the “Super Sea Vixen” would be child’s play if it was done in the design phase.

    I do agree that the Lightning would pose a bit more difficulty, with the circular intake being either enlarged to a greater diameter or reshaped completely.

    Since it would be desired to fit a larger diameter (and more powerful) radar antennae to meet the needs of a multi-role aircraft (if this is instead of the Phantom), then the nose might even be changed to a side-intake type. Whether this is reasonable or not is debatable… just remember that the Chinese actually did this with a cloned Soviet type in the 1980s, so surely the Brits could do it in the early-mid 1960s!

    in reply to: Javelin vs Sea Vixen #1253337
    Bager1968
    Participant

    Looking at the engine dimensions & weights, it looks like the Spey would fit in the Avon spaces on both the Lightning and Sea Vixen.

    With only 65% of the non-reheated fuel consumption, only slightly less non-reheated (and much more reheated) thrust, how about re-engining the Lightning F.6s, and buying the thin-wing, reheated supersonic Sea Vixens (both with Speys) instead of buying the Phantoms?

    That would save money, and allow for continued fighter operations from Hermes and Victorious, thus perhaps saving CTOL carrier aviation in the RN.

    Avon:
    Sea Vixen-mk 208 thrust: 11,250 lb; weight: 2,850 lb; length: 113″; diameter: 41.5″; SFC (specific fuel consumption in [lb fuel/lb thrust/hour]): .86
    Lightning-mk301/302 thrust:12,690 lb (16,360 lb); weight: ~2,900 lb (w/o reheat unit); length: 113″; diameter: 41.5″; SFC .86

    Spey:
    Phantom-mk202 thrust:12,250 lb (20,515 lb); weight: 2,700 lb (4,093 lb w/reheat unit); length: 118″/205″; diameter: 37.5″; SFC: .56

    And for a later upgrade, a reheated version of this engine:
    TF-41 (US-built Spey for A-7E) thrust:15,000 lb; weight: 3,018 lb; length: 103; diameter: 37.5″; SFC: .64
    [probably ~24,000 lb reheat thrust]

    That would have made a nice improvement to both fighters!

    in reply to: Flying Leathernecks Museum #1253341
    Bager1968
    Participant

    Thanks.

    The one in 1986 might have been this one, but it did not have the wing-mounted radome on then.

    Since the engine and cowling were removed for the repairs, I might have confused the type, but the article in the base paper called it a “-1D”. [You know reporters, though… even supposedly aircraft-familiarized ones]

    I was only in the hangar a couple of times, and rarely used the base’s main gate after it was placed for display, so I don’t remember getting a close look after it was completed.

    The squadron that finished (and marked) it was VMFA 531, then flying F/A-18s. They were formed in 1943 as VMF(N)-531, the first USMC night fighter squadron.

    As -121 didn’t fly the night-equipped Corsairs, it is more appropriate for this -5P to carry -531 markings (if it still does). I still grumble though, as all the publicity on it being restored by a USMC squadron only mentioned -531 and -121 not at all!

    in reply to: Flying Leathernecks Museum #1254931
    Bager1968
    Participant

    I remember another Corsair well… my squadron, VMA(AW)-121 [A-6E Intruder] started the restoration on it in 1986 [in our copious free time], but were unable to finish because we deployed into the Pacific Ocean on the CV-61 Ranger.

    Another squadron on the base (MCAS El Toro, in Irvine Ca) took over the job.

    The disappointing part was that it was originally to be painted in the colors we used in the Solomons when we were flying them as VMF-121 [highest kill total of any USMC squadron in WW2]… and when we got back, she had been painted in the other squadron’s markings!

    Oh well, Ce est la Guerre (forgive the atrocious attempt at French).

    MCAS El Toro was closed in the 1990s, and relocated all squadrons to NAS Miramar (which became MCAS Miramar when all the US Navy squadrons went to other USN air stations).

    I could have sworn that the Corsair we were working on was an F4U-1D, but all of those in USN/USMC custody are 2 FG-1Ds [BuNo 92013 & 92246] in the National Museum of Naval Aviation; Pensacola, Florida. They also have an F4U-4 [# 97349].

    The only USMC ones are F4U-4 [# 97369] & F4U-5P [# 122189] (both listed as “USMC Museum” with no location given), and F4U-5NL [# 124447] (Marine Corps Museum; Quantico, Virginia).

    That info is from Flight Journal Special Issue:F4U Corsair (winter 2004), so it should be fairly accurate.

    This raises the questions… as this MCAS Miramar Corsair is obviously a -5 variant, which one is it? And which one was the one in 1986?

    Any help would be appreciated.

    in reply to: Aussie Air Transport Thread #2590088
    Bager1968
    Participant

    And what about the Turkish-built 295 that crashed there?

    in reply to: Different path to V/STOL #2591783
    Bager1968
    Participant

    “The aircraft was not a success.”

    Mainly due to the US Army only giving the manufacturers engines of half the power called for in the design! (in that time, aircraft engines were a “Government Furnished Item”, and you put in what they gave you to put in, regardless of what it was!)

    There were several other unconventional aircraft designs that were “killed” by opponents within the US military forcing them to do their tests with significantly weaker engines than they were designed for. When their performance with the weak engines fell short of the predicted performance (with full powered engines), they were labelled a “failure”, and funding terminated.

    in reply to: Museum P40 #1263979
    Bager1968
    Participant

    I like her this way!!

    While I normally prefer flying restorations, then good static restorations, there is just something so very “right” about the way they have done this display!

    This museum has my great respect, and appreciation for this wonderful job, which captures both the essence of this plane’s service and the passing of time that has made such artifacts into much more than “just old airplanes”!

    in reply to: Scrapping of USS Coral Sea #2052314
    Bager1968
    Participant

    Well, she operated F-18s, so Rafes should be no problem at all!

    in reply to: PA-58 Verdun… #2052359
    Bager1968
    Participant

    Here is the text of the Conway’s article.
    Note that they do state that the PA-58 would have 75m catapults… I guess the artist didn’t read the text!

    In 1958, while Clemenceau and Foch were still under construction, a third carrier was approved. The PA 58 design was larger and heavier, and although it bore a superficial resemblance to PA 54, was clearly influenced by the new ‘super carriers’ built by the US Navy. The shape of the flight deck, which was given considerable overhang on either side amidships, enabled the island to be positioned farther outboard. Parking space amidships was thereby increased, and the 200m hangar was positioned centrally. Two deck-edge lifts, each 17m x 14m, were sited forward and aft of the island to starboard. The length of the catapults was increased to about 75m so that larger aircraft could be handled. They were, however, positioned in the same way as those on Clemenceau so that there was a clear separation between flying operations, which were confined to the port side of the ship, and parking and handling operations. The angled deck measured 192m and was angled at 8° as on Clemenceau.
    The significant increase in power needed to sustain fleet speed led to a corresponding increase in the number of shafts from two to four. Protection of flight deck and machinery was on a similar pattern to Clemenceau, but the thickness of the armour was slightly increased.
    The eight single 100mm of Clemenceau were to be retained but, in addition, it was planned to fit a twin launcher for the new Masurca SAMs on either side of the flight deck aft (as in the US Navy’s Kitty Hawk).
    In addition to Alize ASW aircraft and Etendard fighter-bombers, PA 58 was to operate Mirage IVM heavy strike aircraft. The latter, under development for the Navy since 1956, had a length of 19m, a wing-span of 12m, and a take-off weight of 20t.
    PA 58, possibly to be named Verdun, was delayed by financial problems, and the Defence Staff considered a smaller design, derived from Clemenceau, in which the after guns would have been replaced by Masurca before the project was finally abandoned in 1961.

    in reply to: Neptune Air Tankers #1266249
    Bager1968
    Participant

    Skippy… are you still here? In GJ, Co, USA I mean.

    Yes, I live in Grand Junction…

    Care to meet?

    in reply to: PA-58 Verdun… #2052716
    Bager1968
    Participant

    I have scanned the drawing fron Conway’s here:
    http://s22.photobucket.com/albums/b336/Bager1968/misc%20ships/?action=view&current=PA-58Verdun.gif

    I will copy & post the text from Conway’s Tuesday evening, as I don’t have a good copy myself… but can get it from the Library.

    The ship was actually authorized (1958), but never started due to budget shortfalls.

    It would have been just barely larger than the USN’s modified Essex CVs, but it would have been a better ship, being designed with the angle deck & deck-edge elevators, rather than modified for them.

    in reply to: Porta-aviones Argentino!!! #2052994
    Bager1968
    Participant

    I don’t know… this is what I got from a discussion thread on another board… it may or may not be accurate.

    Of course, the BS-5 designation does apply to the catapults made by Mitchell-Brown, the 52m version could have been installed during a refit… I don’t know.

    The data from that discussion:
    RN
    (BS=Mitchell-Brown), (MS=MacTaggert-Scott)

    Type Run Length Capacity Classes
    MS? ? ? ? Mod Colossus
    BS4 103ft 160ft 40,000lb@78kt Mod Majestics, Centaur, Albion, Bulwark, Hermes
    BS4 145ft 200ft 50,000lb@97kt Mod Hermes, Ark Royal (1960), Victorious
    BS5 151ft 220ft 50,000lb@91kt Eagle 1964, Ark Royal 1970?
    BS5 199ft 268ft 50,000lb@105kt Eagle 1964, Ark Royal 1970?

    MN

    Type Run Length Capacity Classes
    BS5 151ft (46m) 220ft (67m) 50,000lb@91kt / 33,000lb@150kt Clemenceau

    C13(MN) 75m (246ft) 270ft ~70,000lb@140kt CdeG

    Run is the distance the catapult shuttle moves, and Length is the total length of the installation.

Viewing 15 posts - 3,181 through 3,195 (of 3,360 total)