acft japan et al 1970

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  • 8/10/2019 Acft Japan Et Al 1970

    1/1

    FLIGHT international 4 /ur re 97 0

    929

    Kawasaki

    P-2J

    (Two 2,850

    s.p.h.

    IHI/

    General Electric T64-GE-10 turboprops,

    plus two 3,0801b IHI J3-IHI-7C auxiliary

    turbojets). Extensive development of the

    Lockheed Neptune in Japan has resulted in

    the P-2J for the JMSDF, of which 46 are to

    be built by 1974. Main features are an .

    extended forward fuselage for extra ASW

    equipment, larger rudder and redesigned

    main undercarriage with twin wheels, turbo-

    props,

    and new sensor systems. Span, 101ft

    5in; length, 96ft 2in; max gross, 74,9561b:

    long-range cruise, 200kt.

    Mitsubishi Mu-2 (Two 575 s.h.p. AiR e-

    search TPE-331-25A turboprops). Nine

    unpressurised Mu-2Cs are in service with

    JGSDF for liaison, reconnaissance and air

    support, and 17 Mu -2Es, also unpressurised,

    have been delivered to the JASDF for

    search and rescue duties. Span, 39ft 2in;

    length, 33ft 3in; max weight, 8,9301b; max

    cruise, at 10,000ft, 270kt; max range, 1,130

    njn .

    Mitsubishi XT-2

    (Two Rolls-Royee/Turbo-

    meca Adour turbofans giving 6,9501b with

    afterburning). This two-seater supersonic

    trainer with close-support capability was

    designed for a JASDF 1974 requirement,

    the first of two prototypes being due to

    fly in 1971. The typ e.bea rs a quite rem ark

    able resemblance to the Sepecat Jaguar.

    Production of 200 is anticipated. Span, 26ft

    3in; length, 55ft 9in; normal gross,

    21,0001b; max speed, at 33,000ft, Mach

    1.6; ferry range, 1,390 njn.

    NAMC XC-1A

    (Two 14,5001b Pra tt &

    Whitney JT8D-9 turbofans). This high-wing

    tactical transport was designed to meet the

    JASDF's C-X (C-46 replacement) specifica

    tion. The requirement is for about 50, with

    the first of two prototypes to fly this

    summer and service deliveries to begin in

    1973.

    It is an advanced design with full-

    span slats, high-lift flaps, spoilers and T-tail.

    The pressurised fuselage will hold 60 troops,

    a 2i-ton truck, or a 10mm howitzer, with

    access through an under-tail ramp door.

    Span, 101ft 9in; length, 95ft 2in; normal

    payload, 17,6351b, max gross, 85,9801b; max

    cruise, at 35,100ft, 380kt; range, with

    17,6351b payload, 700 n.m.; max fuel range,

    1,800 run.

    NAMC YS-11

    (.Two 3,060 e.h.p . Roll s-

    Royce Dart RDa.10/1 Mk 542 turboprops).

    Nine have been delivered to the Japanese

    Air Self-Defence Force, while the Maritime

    SDF operates a further 3 YS-11M freighters

    with strengthened cabin floors and extra

    freight doors and 4 YS-11T anti-submarine

    trainers. Span, 105ft; length, 86ft 3in; max

    payload, 15,9051b, max gross, 51,0101b; max

    cruise, 252kt; range, with max payload,

    590 n.m., with max internal fuel, 1,140 a m

    Shin

    Meiwa

    PX-S

    (Fou r 2,850 e.s.h.p.

    IHI/General Electric T64-IHI-I0 turbo

    props). The first prototype of this big

    Japanese ASW flying-boat, which uses BLC

    for near-STOL performance, flew in October

    1967. Tw o are in service with the J M SD F

    and 14 are to be delivered by the end of

    1973.

    Span, 107ft 7in ; length, 110ft; m ax

    gross, 86,8601b; max speed, 295kt, approach

    speed, 47kt; max range, 2,560 n.m.

    N E T H E R L A N D S

    Fokker-VFW F.27 Mk 400M Troopship

    (Two 2,210 s.h.p. Rolls-Royce Dart RDa.7

    Mk.532-7 turboprops). Series 400 Friendship

    with accommodation for 45 paratroops, 24

    stretchers with 8 attend ants, a large carg o

    door and 2 parachuting doors. Nine of the

    RNethAF's 12 F.27s are of this type, as

    are four for Sudan and eight for the

    Argentine air forces; the Philippine Air

    Force has a standard model. Span, 95ft 2in;

    length, 72ft 4in; max payload,. 12,8351b,

    max gross, 43,5001b; normal cruise, 256kt;

    range, with max payload, 538 n.m., with

    max fuel and 10,5601b payload, 1,065 n.m.

    P O L A N D

    WSK-Mielec TS-11 Iskra (One Ho-10

    1 7601b turbojet ). Replacement for piston^

    engined TS-8 Bies basic trainer; first

    entered service in 1963 and still in produc

    tion. Holds four Class C-l-d records, includ

    ing 839km/hr (453kt) over 15/25km. Attrac

    tive unswept mid-wing monoplane with

    underslung engine and boom rear fuselage.

    Can have fuselage guns and underwing

    stores. Span, 33ft; length, 36ft 7in; max

    gross, 7,9351b; max speed, at 20,000ft,

    432kt; max range, 540 n.m.

    S P A I N

    CAS A C.207 T.7) Azor

    (Two 2,040 h.p.

    Bristol Hercules 730 radials). Scaled-up

    version of the C.201 twin-engined low-wing

    transport now obsolete. Twenty of the 30-

    pax Azors are in service, half being fitted

    for cargo with a large door. Span, 91ft 3in;

    length, 68ft 5in; max payload, 8,8201b;

    max g ross, 36,3751b; max cruise at 12,340ft,

    216kt; max range with 30 pax, 1,410 n.m,

    with 6,6001b freight, 1,270

    n.m.

    CASA C.212 Avicar

    (Two 755 e.h,p.

    Garrett TPE 331-201 turboprops). A light

    STOL transport designed to replace the

    Spanish Air Force's fleet of Ju52/3M;

    DC-3 and C.207s. High-wing monoplane

    with ramp under rear fuselage for vehicle

    loadin g; 16 paratr oops , 12 stretchers or 18

    civil pax. Funds for two prototypes, 1970

    first flight, and a production contract being

    negotiated. Span, 62ft 4in; length, 49ft 9in;

    max payload, 4,4101b; max gross, 13,2301b;

    max cruise, at 12,000ft, 198kt; max range,

    1,145 n.m, with max payload, 325

    n.m.

    Hispano

    HA-200E

    Super Saeta

    (Two

    1 0581b

    Turbomeca M arbore V I turbojets).

    Tandem-seat low-wing monoplane basic

    tra ine r: 5 protot ypes, 30 HA-200A and 55

    HA-200D built for Spanish Air Force. Ten

    HA-200B built for Egypt, with 90 being

    built under licence. In the HA-200E, for

    Spain, the Marbore VI replaces the less

    powerful Marbore IIA, electronics have

    been modernised and two Matra 38 weapon

    mo untin gs are fitted. Span, 35ft lOin; length ,

    29ft 5in; max gross, 7,9371b; max range,

    at 30,000ft, 810 n.m.

    S W E D E N

    MFI-9B Militrainei

    (One 100 h.p. Rolls-

    Royce Continental O-200-A). Development,

    by its original designer, of the Bolkow

    Junior, which was evaluated by the Swedish

    Air Force and was used by Biafra during

    the Nigerian civil war. Wing hard points

    allow the carriage of six 7.5cm RP, two

    Bofors Bantam teleguided missiles, or 18

    37mm rockets. Span, 24ft 4in; length, 19ft

    2in; max gross,

    1 2701b;

    max speed,

    130kt; max range with full payload, 435

    MFI-10B Vipan

    (One 180 h,p. Lycoming

    O-360-A1A). High-wing four-seater liaison

    type designed for the Swedish Air Board.

    Production seems unlikely. Span, 35ft 3in;

    length, 25ft llin; max gross, 2,5901b; max

    speed, at 7,000ft, 12 7kt; max ra nge , 540

    Above one of nine Mitsubishi Mu-2Cs of

    the JGSDF used for l iaison an d reconnaissance.

    Right Japanese -built F-I04J at Chitose air

    base. Note fuselage pylon for stores

    8fAK-