Catalog excerpts
TURBOSHAFT ENGINE Designed for small helicopter applications.
Open the catalog to page 1
Main parameters – performance (ISA SL) Main features TS 100ZA Output shaft speed Dimensions and weight Weight (dry) Engine length Width × depth (without exhaust) Applies to standard ISA (101. 325 kPa, t0 = 15O C, v0 = 0 km/h) Mode Output shaft power Fuel consuption (SFC) kg/kW/h • Small installation dimensions, low weight and high static power • Gearbox design offers the possibility to install a high speed electric generator with output power 3,0 kVA • Modular conception with gas generator, power turbine and gearbox • Standard completation: fuel-oil system, control system, ignition unit,...
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