Lockheed 1329 JetStar I / II
1957
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Lockheed VC-140B Jetstar

To meet a US Air Force requirement for an 'off-the-shelf' high-performance light transport, Lockheed developed the Lockheed 1329 JetStar. A clean low-wing monoplane with swept wings and swept tail surfaces, the JetStar was powered in prototype form by two 2200kg thrust Bristol Orpheus 1/5 turbojet engines. The first of two prototypes was flown on 4 September 1957, with flight testing proving satisfactory, but when planned licence-production of the Orpheus engine could not be finalised, Lockheed chose instead to power the initial production version by four 1361kg thrust Pratt & Whitney JT12A-6 engines, mounted in pairs on each side of the rear fuselage. The anticipated military demand failed to materialise in any significant numbers, with the result that the majority of the 204 JetStars that were built, before production ended in 1980, were sold as business/executive aircraft.

Variants:

JetStar I: original production version, differing from the first prototype by having increased fuel capacity provided by a permanently attached streamlined JuelI tank at mid-span of each wing, de-icing of wing and tail unit leading edges and Pratt & Whitney JT12A-6 engines; a slightly lengthened fuselage provided executive standard accommodation for a crew of two and 10 passengers; late production aircraft had 1497kg thrust JT12A-8 turbojet engines

JetStar 731: conversion developed by AirResearch, replacing the Pratt & Whitney powerplants of Jet Star I aircraft with more fuel-efficient Garret TFE731-1 turbofan engines; about 60 JetStar Is were converted to this standard

JetStar II: new production version incorporating Garrett TFE731-3 engines as standard and a number of refinements

C-140A: five aircraft for USAF, basically similar to early production JetStar Is and equipped for calibration of navigation beacons

C-140B: convertible cargo/passenger version for USAF, five built; otherwise generally similar to C-140A

VC-140B: designation of six additional production aircraft, generally similar to C-140A, except equipped as VIP transports; the five C-140Bs were also converted to this configuration

3-View 
Lockheed Jetstar IIA three-view drawing of Lockheed Jetstar II (1280 x 762)


Specification 
 MODELLockheed JetStar II
 ENGINE4 x Garrett TFE731-3 turbofans, 1678kg
 WEIGHTS
    Take-off weight20185 kg44501 lb
    Loaded weight11294 kg24899 lb
 DIMENSIONS
    Wingspan16.59 m54 ft 5 in
    Length18.41 m60 ft 5 in
    Height6.22 m20 ft 5 in
    Wing area50.4 m2542.50 sq ft
 PERFORMANCE
    Max. speed880 km/h547 mph
    Ceiling13105 m43000 ft
    Range4820 km2995 miles

Comments 
Todd Wheaton, TWheaton1961(@)netscape.com, 22.05.2007

Great drawing. However, this is the 731 or "Jetstar II". The L-1329 was powered by JT-12's and the engine nacelles were considerably smaller and the fuel tanks, although located in the same region span-wise, were not "slung" under the wing like the 731, but split the wing top to bottom 50/50.

I could use a really good three-view of the Dash-8, or L-1329 Jetstar as the original was known.

Thanks,

Todd

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