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The United States Navy in the Cold War Era: What ifs.

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  • The United States Navy in the Cold War Era: What ifs.

    (Primary source material is the 13th Edition of the Ships and Aircraft of the U.S. Fleet by Norman Polmar and the Naval Historical Center)

    Heavy Aircraft Carrier (CVA) On 29 July 1948, construction of five "supercarriers", for which funds had been provided in the Naval Appropriations Act of 1949. The keel of the first of the five planned postwar carriers was laid down on 18 April 1949 at Newport News Drydock and Shipbuilding. The program was canceled on 23 April 1949, United States was not completed, and the other four planned carriers were never built.

    The primary drive behind the design was the development of a carrier using the new jet aircraft. The new jets were faster, larger and much heavier that the WW2-era aircraft used on the Essex and Midway-class carriers. It was anticipated that the aircraft would have a much longer range thus allowing the carrier to operate further away from any targets. These requirements would require that the ships strength deck would have to be the flight deck rather than the hanger deck as in traditional US carrier design. The heavier flight deck meant that the ship would have a greater tendency to roll in rough seas, since a much larger part of the ships weight would be high above the waterline.

    Due to the anticipated size of the new aircraft, the CVA would be flush-decked, meaning that the design would have no island superstructure. This resulted in two major concerns;

    1) How would the exhaust gas from the power plants be diverted from the flight deck The USNs first carrier, USS Langley, had been built flush-decked and this problem caused a great many problems that were never satisfactory resolved.

    2) Were are the necessary radar equipment to be mounted One possible solution was for a command ship to remain close by, carrying the task force commander and the necessary radar equipment. The USS Northampton (CLC-1) would be built to fulfill this mission. Another solution was for an airborne early warning radar to be carried among the air group.

    It was finally assumed that the CVA would not operate by itself, but in conjunction with traditional fleet carriers as a complementary bomber-carrier. There was a great deal of debate on the CVAs mission. One viewpoint was that the ship would carry a group of large bombers that would be secured to the flight deck with no hanger space as the bombers would be too large to be moved via the ships elevators. This allowed for munition to be reduced as multiple strikes would be unlikely. A hanger area for a small fighter contingent and a small magazine for nuclear weapons storage were provided.

    The final design included a more balanced air group but would be able to support the heavier nuclear-armed bombers. It would be equipped with four deck edge elevators (three waist and one stern) as well as four catapults (two forward and two waist). The CVA would be able to launch and simultaneously recover aircraft. Estimated cost was $189 million dollars (equivalent to $1.66 billion in 2020).

    Unfortunately, the CVA concept as a nuclear-armed bomber carrier was viewed as a challenge to the USAFs monopoly on strategic nuclear weapons delivery.

    Looking to cut the military budget and accepting without question the Air Force argument on nuclear deterrence by means of large, long-range bombers, Secretary of Defense Louis A. Johnson announced the cancellation of construction of United States, on 23 April 1949, five days after the ship's keel was laid. Secretary of the Navy John Sullivan immediately resigned, and Congress held an inquiry into the manner and wisdom of Johnson's decision. In the subsequent "Revolt of the Admirals" the Navy was unable to advance its case that large carriers would be essential to national defense.
    Soon afterward, Johnson and Francis P. Matthews, the man he advanced to be the new Secretary of the Navy, set about punishing those officers that let their opposition be known. Admiral Louis Denfeld was forced to resign as Chief of Naval Operations, and a number of other admirals and lesser ranks were punished. The invasion of South Korea six months later resulted in an immediate need for a strong naval presence, and Matthews' position as Secretary of the Navy and Johnson's position as Secretary of Defense crumbled, both ultimately resigning.

    Displacement: 66,000 tons standard, 83,000 tons full load. Length: 1,030ft (314m) at waterline; 1,088ft (331.7m) overall Beam: 125 feet (38.1m) Flight Deck: 190 ft (57.9m) Propulsion: (8) 1,200psi Foster-Wheeler boilers; (4) Westinghouse steam turbines totaling 280,000shp; driving four screws. Speed: 33 knots Range: 12,000nm at 20kts Crew: 3,019 officers and enlisted, 2,480 air wing officers and enlisted, total of 5,499 officers and enlisted Armament: (8) 5in/54 caliber guns in single mounts; (16) 3in/70mm AA guns in eight twin mounts; (20) 20mm/70 autocannons (single, dual or quad mounts were debated).
    The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

  • #2
    USN What ifs Part Two

    Sea Control Ship (SCS) In the late 1960s, studies by US Navy identified a potential requirement for large scale convoy operations in the event of a war with the Soviet Union. In order to compensate for a shortage of escort ships, it was suggested that helicopters operating from small helicopter carriers could fill the gap. When Elmo Zumwalt became Chief of Naval Operations in 1970, he seized on the idea of small helicopter carriers as part of his "High-Low" plan in which large numbers of cheaper lower capability ships would be built to supplement existing expensive high capability ships. The proposed small carrier, which was named the Sea Control Ship (SCS), was required to provide continuous airborne cover of two anti-submarine and one airborne early warning helicopters, as well as carrying VSTOL fighters to stop Soviet long-range aircraft (like the Tupolev Tu-95 "Bear") from shadowing convoys and directing submarines and surface ships against them. This resulted in a requirement to carry 14 helicopters and three VSTOL fighters such as the AV-8 Harrier. It was hoped that production SCSs could be built for $100 million each, an eighth of the price of a full sized aircraft carrier.
    In 1971 USS GUAM (LPH-9), was used as a test vessel. Testing began on 18 January 1972. In 1974 she was deployed to the Atlantic Ocean. The vessel was equipped with AV-8A Harrier STOVL fighters and SH-3 Sea King ASW helicopters. The tests were completed in July 1974.
    The lead ship was planned for the fiscal year 1975 shipbuilding program. However, Congress refused to authorize the ships because of their limited capability and strong opposition by the advocates of large carriers. The SCSs were smaller than most fleet aircraft carriers, and the concept was seized upon by nations wanting inexpensive aircraft carriers. Spain's PRINCIPE DE ASTURIAS, and her smaller cousin ship, Thailand's HTMS CHAKI NARUEBET, were based on the final US Navy blueprints for a dedicated sea control ship, but with the addition of a ski-jump ramp and follow a similar mission profile.

    Displacement: 9,770 tons light; 13,735 tons full load Length: 620ft (190m) Beam: 80ft (24m) Draft: 21.62ft (6.59m) Propulsion: (2) General Electric LM2500+gas turbines, single shaft, 45,000shp; (3) 2500Kw ship service generators. Speed: 26kts; 24kts sustained Crew: 76 officers, 624 enlisted Armament: Two Mk15 Phalanx CIWS Aircraft Carried: (3) AV-8A Harrier VTOL; (17) SH-3 Sea King ASW helicopters
    Aviation Facilities: Flight Deck: 545 x 105ft (166.1 x 32m) Enclosed Hanger: 19ft (5.8m) high Aircraft Elevators: 60,000lb (27.2mt) lift capacity Centerline: 60x30ft (18.3x9.1m) Stern: 35x50ft (10.7x15.4m) JP-5 Fuel Capacity: 950 tons (861.8mt) Aviation Ordnance: 180 tons (163mt)
    The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

    Comment


    • #3
      USN What Ifs Part Three

      VSTOL Support Ship During the mid-1970s there was increased USN interest in VSTOL aircraft, with a major analysis known as the Sea-Based Air Master Study developing a long-term program for several categories of VSTOL aircraft.
      Admiral Zumwalt's successor as CNO, James L. Holloway III abandoned plans for the SCS and instead proposed a larger and faster design, the VSTOL Support Ship, or VSS. By June 1976, it was planned that the VSS would be 690 feet (210 m) long and would be powered by four General Electric LM2500 gas turbines driving two propeller shafts (essentially double the machinery of the single shaft SCS) which would give a speed of 29 knots (54 km/h; 33 mph). It would carry 22 helicopters (16 H-53 Sea Stallions and six LAMPS light helicopters) together with four Harriers. Holloway hoped to develop a series of advanced V/STOL aircraft, including a supersonic fighter and a utility aircraft for Anti-Submarine and Airborne Early Warning duties which could operate from the VSS as well as from the Navy's existing carriers, although these types were never fully defined. The need to accommodate the new designs resulted in the carrier's design being reworked in February 1978 as the VSS II. This design had a larger hangar and greater beam than the original design to allow the potentially larger advanced aircraft to be carried, and carried substantially more aviation fuel.
      A third variant, the VSS III, evolved by July 1978 as a result of a requirement to protect the ship's magazines. In order to cope with the extra weight of the armor, the ship had a new hull form with less freeboard but allowing greater speed. The final VSS III design was 717 feet (218.5 m) long overall and 690 feet (210.3 m) at the waterline, with a beam of 178 feet (54.3 m) and a draft of 24 feet 4 inches (7.42 m). Displacement was 20,116 long tons (20,439 t) light and 29,130 long tons (29,600 t) full load. As well as the ship's aircraft, two quadruple Harpoon anti-ship-missile launchers were to be mounted on the fantail, with two Phalanx Close-in weapon systems were to be fitted. A complement of 49 officers and 910 other ranks were to operate the ship while the ship's air wing had 87 officers and 541 other ranks. The final configuration is described below.

      Displacement: 20,115 tons light; 29,130 tons full load Length: 690ft (210.4m); 717ft (218.6m) oa Beam: 178ft (54.3m) Draft: 25.5ft (7.7m) Propulsion: (4) General Electric LM2500 gas turbines; 2 shafts; 90,000shp Speed: 30kts Manning: 97 officers and 910 enlisted, air group of 87 officers and 541 enlisted; total of 184 officers and 1,451 enlisted. Armament: (2) Mk15 Phalanx CIWS Air Group: 8 AV-8A Harrier VTOL; 6 SH-2F Sea Sprite and 16 SH-3 Sea King ASW helicopters
      The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

      Comment


      • #4
        USN What Ifs Part Four

        Medium Aircraft Carriers In the early 1970s, the United States Navy, following the doctrine of Chief of Naval Operations Admiral Elmo Zumwalt for larger numbers of smaller and cheaper ships, initiated design studies for a "minimum-cost" carrier of 50,00060,000 tons. The new design was planned to be much cheaper than nuclear-powered carriers (a cost target of $550 million was set in 1972) but still be suitable for replacing the ageing Midway-class aircraft carriers. Work on the project (designated T-CBL) was stopped however, when the US Congress made statements encouraging all major warships to be nuclear-powered, and in 1976 an order was placed for a fourth nuclear-powered Nimitz-class aircraft carrier.

        Later that year, however, US President Gerald Ford cancelled the order for the fourth Nimitz, stating that instead, two CVVs, medium-sized, conventional-powered carriers which were expected to mainly operate V/STOL aircraft would be built. The existing T-CBL design formed the basis for the new CVV, this being of the required size, while capable of operating all existing conventional carrier aircraft (this proved important as the hoped-for supersonic V/STOL fighters did not come to fruition).

        The CVV carried a smaller air group than existing supercarriers (i.e. about 60 compared with about 90 for the nuclear-powered Nimitz class or the conventional-powered Kitty Hawk-class aircraft carriers) and had two steam catapults rather than four, and three arrestor cables instead of four. The CVV also had a less powerful power plant, with steam turbines fed by six boilers generating 100,000 shaft horsepower (75,000 kW) in a two-shaft arrangement, compared with the 280,000 shaft horsepower (210,000 kW) delivered to four shafts of the larger carriers, giving a speed of 28 knots (52 km/h) compared with over 31 knots (57 km/h). While slower than earlier carriers, this was still sufficiently fast to keep up with carrier task forces. Not all of the design features in the CVV were less capable than earlier carriers, however, as the carrier was planned to have improved protection for the ship's magazines and to be protected against under-keel explosions.

        The Carter administration from 1977 onwards continued with the CVV program, by now expected to cost $1.5 billion per ship compared to $2.4 billion for a Nimitz, vetoing congressional attempts to vote $2 billion towards construction of a fourth Nimitz, although plans for a second CVV were abandoned. When it was realized that a repeat of USS John F. Kennedy, the last conventionally powered large carrier to be built would only cost about $100 million more than the CVV, while being much more capable, the Navy and the Secretary of Defense Harold Brown recommended that a repeat John F. Kennedy be included in the 1980 shipbuilding program instead of the CVV, but this was rejected by Carter, partly based on the lower life-cycle costs of the smaller ship with its smaller airwing. Following is the design Congress was willing to accept; however, the ship was strongly opposed by proponents of the nuclear-powered NIMITZ, especially Admiral Rickover, and none were authorized.

        Displacement: 52,200 tons standard; 62,427 tons full load Length: 912ft (278m) waterline; 923ft (281m) overall Beam: 126ft (38m) waterline; 256.5ft (78.2m) flight deck Draft: 34ft (10m) Propulsion: (2) steam turbines; (2) shafts; 100,00shp Speed: 27.8kts Range: 8,000nm Crew: 4,025 (including air wing) Armament: (3) MK15 Phalanx CIWS Aircraft: 55-65
        The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

        Comment


        • #5
          USN What Ifs Part Five

          Strike Cruiser The strike cruiser (CSGN) was an outgrowth of the DLGN concept, developed in 1973-1974 as an enlarged DLGN intended to specifically to carry the Aegis weapon system. As more weapons were added (Harpoon and Tomahawk missiles) the ship was enlarged and the twin reactor D2G propulsion plant was upgraded.

          The basic CSGN design was an improved CGN-38 class hull with several thousand tons of armor added. This would have been the first armored ship built by the USN since the USS LONG BEACH. The additional displacement would have reduced speed to 28-28.5kts; accordingly, the design was lengthened until at least 30 knots could be achieved, resulting in a very shallow draft.

          Initially the ship was to only carry the Phalanx CIWS; however, in an effort to make the ship more competitive than the proposed Aegis-armed destroyer (DG/Aegis and later DDG/CH-47), an 8-inch Mk71 Lightweight Gun was fitted forward.

          The ship was proposed as a carrier escort, with up to four CSGNs being considered to screen each carrier. The cost of the lead strike cruiser in fiscal 1976 was estimated $1.371 billion and she was to be have been completed in December 1983.

          After the initial concept was ignored by Congress, the Naval Sea Systems Command hurriedly developed a Strike Cruisers Mark II design retaining the same armament but adding a flight deck, presenting a superficial similarity to the Soviet KIEV class VTOL carriers. However, the U.S. ship, with two Mk26 launchers and two 8-inch lightweight guns, would have had an enlarged island structure incorporating hangers for six AV-8A/B Harriers VTOL fighters and three SH-60 ASW helicopters. A further modification to the Mark II design considered a hanger below the flight deck, resulting in a design somewhat similar to the Navys light carrier of World War Two (CVL 22-30). That design would have carried about 18 Harriers on a displacement of 18,000 tons. Below is the Mark II stats:

          Displacement: 15,900 tons standard; 17,210 tons full load Length: 666ft (203.1m) waterline; 709ft 7in (216.28m overall Beam: 76ft 5in(23.29m) Draft: 22ft 4in (6.81m) Propulsion: (2) pressurized water D2G General Electric nuclear reactors, (2) shafts, 60,000shp
          (2) 2,000 kW (2,700 hp) diesel generators (6) ship service turbo generators Speed: 30+ knots Crew: 454 Armament: (2)2 Mk26 missile launchers with SM2MR Block III/IV SAMS and ASROC 64 missiles forward, 64 missiles aft (4)2 Mk143 Armored Box Launchers each with 4 BGM-109 Tomahawk missiles
          (4)4 Mk141 Launchers, each with 4 RGM-84 Harpoon missiles (1)1 8/55 caliber MCLWG (forward) (2) Mk15 Phalanx CIWS (midships) (3)2 Mk32 SVTT with Mk46 ASW torpedoes Air Group: (6) AV-8A/B Harrier VTOL; (3) SH-60B ASW helicopters
          The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

          Comment


          • #6
            USN What Ifs, Part Six

            Typhon-class Frigate In the early 1960s, the USN planned to construct a class of at least seven DLGNs fitted with the Typhon AAW system. The Typhon consisted of an advanced radar/fire control system plus a medium-range missile to replace the Terrier and long-range missile to replace the Talos then being fitted to U.S. warships. Construction of the lead ship was to begin in 1963-64.

            The high costs of the Typhon DLGN led Secretary of Defense McNamara to cancel the program late in 1963. The systems SPG-59 fixed-array search/tracking radar was tested in the guided missile ship NORTON SOUND (ABM-1). Several Typhon concepts and features were later incorporated into the subsequent Aegis system.

            Displacement: 9,750 tons standard; approx.. 12,000 tons full load Length: 650ft (198.2m) waterline Beam: 64ft (19.5m) Draft: 21ft (6.4m) Propulsion: (2) pressurized-water D2G reactors; 2 shafts Speed: 30+ knots Crew: approx. 500 Missiles: (2)1 Typhon long-range launcher (60 missiles) (1)2 Typhon medium-range launchers (80 missiles each) (1)2 Mk42 5in/54mm guns (one fore and aft) ASW Weapons ASROC fired from Typhon ling-range launcher (3)2 12.75in (324mm) torpedo tubes with Mk46 ASW torps
            The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

            Comment


            • #7
              Thanks for these Dragoon! Keep them coming!

              Have you looked at Norman Friedman's Illustrated Design History series of books They are excellent and have tons of details on these programs.
              I love the smell of napalm in the morning. You know, one time we had a hill bombed, for 12 hours. When it was all over, I walked up. We didn't find one of 'em, not one stinkin' body. The smell, you know that gasoline smell, the whole hill. Smelled like... victory. Someday this war's gonna end...

              Comment


              • #8
                Originally posted by chico20854 View Post
                Thanks for these Dragoon! Keep them coming!

                Have you looked at Norman Friedman's Illustrated Design History series of books They are excellent and have tons of details on these programs.
                working on acquiring the series, but I do favor Polmar's works, bit more balanced.
                The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

                Comment


                • #9
                  I saw the model or photo of the model for the Strike Cruiser mkII in the '80s and thought it was f'in awesome! A self defending CV. Would love to see a modern version for carrying F-35s. Impractical, but cool.
                  If you run out of fuel, become a pillbox.
                  If you run out of ammo, become a bunker.
                  If you run out of time, become a hero.

                  Comment


                  • #10
                    The DG(Aegis)

                    A large number of destroyer designs were developed by the USN from the 1950s onwards. The current Aegis program (manifested in the CG-47/DDG-51 designs) originated in 1963 with the Advanced Surface Missile System (ASMS). As the development of the large Typhon missile frigate (DLGN) began to encounter difficulties, the ASMS effort was undertaken, partially based on the expectations of new solid-state electronics.

                    The development was protracted and in 1971 the Chief of Naval Operations, Admiral Zumwalt, directed a design effort to provide the smallest possible ship that could carry the new air-defense weapons/electronics system. The initial goal was a displacement of 5,000 tons, but that was soon raised to 6,000 tons. Several designs were put forward, with the more austere versions having a single Mk26 Mod 1 missile launcher for surface-to surface missiles as well as ASROC, a small sonar and a helicopter landing deck but no hanger. By early 1973, the design had been recast, with two Mk13 launchers (a total of 80 missiles but no ASROC capability), plus a full LAMPS facility for one helicopter. The desire for longer-range as well as nuclear SAMS led to still another recasting, this time to provide the Mk26 Mod 2 launcher (with 64 missiles).

                    However, congressional confusion, the change of the CNO in mid-1974, and advocacy of an all-nuclear Aegis by Admiral Rickover led to the demise of the DG(Aegis) in favor of various DLGN-type designs as well as the CSGN strike cruiser.

                    The ARLEIGH BURKE-class represents a return to the DG(Aegis) concept. The availability of the vertical-launch missile system (90 weapons) and improvements in the SPY-1 radar coupled with the deletion of the LAMPS helicopter facilities as well as one 5-inch gun permit the construction of a smaller Aegis ship, as envisioned in the early 1970s.
                    The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

                    Comment


                    • #11
                      The FFX

                      During the late 1970s, the Navy proposed the construction of a class of small frigates (FFX) for use by the Naval Reserve Force. These ships were intended to augment the Olive Hazard Perry-class ships in the ASW role in low-threat areas. A class of approximately twelve ships was planned with the lead ship intended for authorization in FY 1984. For reasons not fully clear, although such ships would have had marginally effective ASW capabilities, the FFX class was not started. Subsequently, the Naval Reserve Force has been provided with frigates of the Knox and Perry-classes to replace their current aging Gearing-class ships.

                      Known characteristics include a full load displacement or 2,000---2,400 tons; a speed of 25 knots; a range of 5,000nm at 16---18knts; a crew of 120 men; facilities for one SH-2F LAMPS I; provisions for two triple Mk32 324mmTT w/Mk46 ASW torps; gun armament included a single Mk42 5in/54 gun and a Mk15 Phalanx CIWS.
                      The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

                      Comment


                      • #12
                        The Sea Frigate

                        During the late 1970s, the Navy planned to construct a class of Surface Effect Ship (SES) frigates in the mid-1980s. These ships were to be based on a 3,000-ton SES prototype that was to be constructed in 1980-1984. This ship was to have been capable of speeds as high as 80 to 100 knots with a trans-ocean design and to have carried frigate-type weapons, including two LAMPS helicopters.

                        The Secretary of Defense decided in May 1976 to proceed with the design and construction of a 3,000-ton, oeweaponized prototype SES. This followed 10 years of extensive conceptual and technical development. A contract for design with an option to construct was awarded in December 1976 to Rohr Marine, Inc. of San Diego. The ship was to be completed during FY 1983. Subsequently, the Carter Administration cancelled the SES program in its entirety.

                        In addition to high speed, the SES program offered a large amount of usable space which would have provided flexibility in the installation of weapons and sensors, with ample space to hangar and operate two helicopters. Also, the design provided considerable stability in heavy seas.

                        Displacement: 3,000 tons full load Length: 270ft (82.3m) oa Beam: 108ft (32.9m) Draft: 14ft (4.3m) on cushion; 31ft (9.5m) off cushion Propulsion: (4) Pratt & Whitney FT9 gas turbines; (4) waterjet propulsion units; (2) General Electric LM2500 gas turbines; (6) lift fans Speed: 80+kts on cushion Crew: 125 Helicopters: 2 SH-2 Sea Sprite LAMPS III Weapons: oeFF/FFG weapons suite
                        The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

                        Comment


                        • #13
                          Little Known Command Ships

                          The USN built one ship and converted another specifically for use as major command ships, while a third such ship was planned for conversion.

                          The heavy cruiser NORTHAMPTON (CA-125), cancelled in 1945 while under construction , was subsequently in 1948 as a tactical light command ship (CLC-1) and completed in that configuration in 1953. After operating as a fleet flagship, she was reconfiguration to serve as a National Emergency Command Post Afloat (NECPA) in 1961 and re-classified as CC-1. She was decommissioned in 1970 and laid up in reserve until stricken in 1977.

                          The light carriers WRIGHT (originally CVL-49) and SAIPAN (CVL-48) were similarly designated for conversion to the NECPA role. The WRIGHT, also designated AVT-7 while in reserve, was converted in 1962-1963 and became CC-2; she operated in the NECPA role until 1970 when she was laid up in reserve. She was stricken in 1977.

                          The SAIPAN, designated as AVT-6 while in reserve after World War Two, began conversion too CC-3 in 1964, but was instead completed as a major communications relay ship in 1966 (renamed ARLINGTON and classified AGMR-2).

                          In the NEPCA role these ships were to provide afloat facilities for the President in the event of a national emergency or war.
                          The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

                          Comment


                          • #14
                            Originally posted by dragoon500ly View Post
                            The USN built one ship and converted another specifically for use as major command ships, while a third such ship was planned for conversion.

                            The heavy cruiser NORTHAMPTON (CA-125), cancelled in 1945 while under construction , was subsequently in 1948 as a tactical light command ship (CLC-1) and completed in that configuration in 1953. After operating as a fleet flagship, she was reconfiguration to serve as a National Emergency Command Post Afloat (NECPA) in 1961 and re-classified as CC-1. She was decommissioned in 1970 and laid up in reserve until stricken in 1977.

                            The light carriers WRIGHT (originally CVL-49) and SAIPAN (CVL-48) were similarly designated for conversion to the NECPA role. The WRIGHT, also designated AVT-7 while in reserve, was converted in 1962-1963 and became CC-2; she operated in the NECPA role until 1970 when she was laid up in reserve. She was stricken in 1977.

                            The SAIPAN, designated as AVT-6 while in reserve after World War Two, began conversion too CC-3 in 1964, but was instead completed as a major communications relay ship in 1966 (renamed ARLINGTON and classified AGMR-2).

                            In the NEPCA role these ships were to provide afloat facilities for the President in the event of a national emergency or war.
                            Some more on CC-1, the Northampton is here.

                            I'm going to weave a similar concept into the history thread, stay tuned!!!
                            I love the smell of napalm in the morning. You know, one time we had a hill bombed, for 12 hours. When it was all over, I walked up. We didn't find one of 'em, not one stinkin' body. The smell, you know that gasoline smell, the whole hill. Smelled like... victory. Someday this war's gonna end...

                            Comment


                            • #15
                              Bell XV-15A

                              A precursor to the V-22 Osprey, the Bell XV-15A is a tilt-rotor technology demonstration aircraft. This was an early entry in the Joint Service Advanced Vertical Lift Aircraft program of the early 1970s. Considered to be the second successful experimental tiltrotor aircraft and the first to demonstrate the concept's high speed performance relative to conventional helicopters. One of the major problems with the early tiltrotor aircraft designs was that the driveshafts carrying power from the fuselage out to the wingtip rotors, along with the gearbox and tilting mechanisms at the wingtips, had substantial loads placed upon them and were heavy. They were transferring large amounts of power and torque long distances for an aircraft power transmission system.

                              The XV-15 experimental aircraft introduced a major design concept advance: instead of engines in the fuselage, the XV-15 moved the engines out to the rotating wingtip pods, directly coupled to the rotors. The normal path for power was directly from the engine into a speed-reduction gearbox and into the rotor/propeller without any long shafts involved. There was still a driveshaft along the wings for emergency use to transfer power to the opposite rotor in case of engine failure, but that shaft did not normally carry any power loads, making it lighter.

                              The tilting engine concept introduced complexities in the design of the engines and engine pods to be able to shift from operating horizontally to operating vertically. Those problems were addressed fairly early in the XV-15 program.

                              The XV-15 first flew on 3 May 1977. Flowing wind tunnel and flight testing by Bell at the Ames Research Center in Mountain View, California the aircraft was moved to NASA Dryden at Edwards Air Force Base, California. The XV-15 flight testing continued expanding its flight envelope. It was able to successfully operate in both helicopter and normal aircraft flight modes and smoothly transition between the two. Once the aircraft was considered sufficiently tested, it was returned to Ames Research Center for further testing.

                              Its first public appearance was at the 1981 Paris Air Show where it was the hit of the show with its maneuverability wowed the audience. The XV-15s were a standard demonstration in the annual summer airshow at the co-located Moffett Field Naval Air Station for several years during the 1980s. Both XV-15s were flown actively throughout the 1980s testing aerodynamics and tiltrotor applications for civilian and military aircraft types that might follow, including the V-22 and AW609 program.

                              The first XV-15 prototype aircraft, N702NA, was transferred back to Bell for company development and demonstration use. On 20 August 1992, the aircraft crashed while being flown by a guest test pilot. He was lifting off for a final hover when a bolt slipped out of the collective control system on one pylon, causing that rotor to go to full pitch. The aircraft rolled upside down out of control and crashed inverted. While significantly damaged, the aircraft was largely structurally intact and both the pilot and copilot escaped with only minor injuries from the crash. The cockpit of the aircraft was salvaged and converted for use as a flight simulator.

                              The second XV-15 prototype, N703NA, was used for tests to support the V-22 Osprey military tiltrotor program and Bell/Agusta BA609 civilian medium tiltrotor transport aircraft. It continued in primarily NASA test operations until September 2003. The shortest takeoff distance was achieved with the nacelles at 75 degrees angle.

                              The Fdration Aronautique Internationale classifies the XV-15 as a Rotodyne, and as such it holds the speed record of 456 kilometers per hour (283 mph), and the 3 km and 6 km time-to-climb.

                              SPECIFICATIONS
                              Crew: 2
                              Capacity: up to 9 passengers if seats fitted/3,400lbs (1,542kg) max payload STOL
                              Width: 57ft 2 in (17,42m overall with rotors turning
                              Height: 12ft 8in (3.86m) over tail fins. 15ft 4in (5m) with nacelles vertical
                              Wing Area: 169 sq ft (15.7 square meters)
                              Empty Weight: 9,570lbs (4,341kg)
                              Gross Weight: 13,000lbs (5,897kf) VTO
                              Max. Takeoff Weight: 15,000lbs (6,804kg) STO
                              Fuel Capacity: 229 US gal (867L) in four wing tanks
                              Powerplant: 2 -- Textron Lycoming LTC1K-4K turboshaft / turboprop engines, 1,550 shp (1,160 kW) each normal takeoff power (10 min max)
                              Main Rotor Diameter: 2x25ft (7.6m)
                              Main Rotor Area: 981.8sq ft (91.21 square meters) total
                              Max. Speed: 332knts (615km/h) at 17,000ft (5,182m)
                              Cruise Speed: 303kts (561km/h) at 16,500ft (5,029m)
                              Never Exceed Speed: 364kts (674km/h)
                              Range: 445nm (824km) with max fuel
                              Service Ceiling: 29,000ft (8,800m)
                              Service Ceiling OEI: 15,000ft (4,572m)
                              Hover Ceiling IGE: 10,500ft (3,200m)
                              Hover Ceiling OGE: 8,650ft (2,637m)
                              Rate of Climb: 3,150ft/min (16.0m/s) at sea level
                              The reason that the American Army does so well in wartime, is that war is chaos, and the American Army practices chaos on a daily basis.

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