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HKS APSU - HKS 700T
Test Lab Photos, July 2008, HKS Aviation LTD Japan


Listen and view an Interview with Dr James Waterhouse of APSU, Quasar Lite Design Engineer, talk about the HKS 700T at Oshkosh 2008 

Specifications
(Down Load / View Technical Specification Sheet)

HKS 700T

 

 

 View the overall 700T dimensions  

Configuration

 

2 Cylinders 4-Stroke Engine With Horizontally Opposed Cylinders 4 Valves per Cylinder Turbocharger with Intercooler

Bore X Stroke

85mm x 62.5 mm

Compression Ratio

8.8 : 1

Power Output

77hp (57.4kw) at 4900rpm (continous)
80hp (59.7kw) at 5300rpm (3min./Take off)

Torque Max

11kg-m at 4600-5200rpm

Max RPM

5300 rpm

TBO

500 hours (Expect higher TBO with fleet experience)

 

Integrated Reduction Gearbox

 

Gearbox type

Reduction Ratio

C-type

2.62

 

Weights

Engine
(Dry, with Electric Starter,
Fuel line with Injector,
Exhaust Manifold, Intake Manifold, turbocharger, and Gearbox)

57.5 kg (126.8 lbs)

HKS 700T Display Unit Photos - Olney September 2008 ASC Nationals
 



Information subject to change, return to this site for updates.