Microturbo TRS 18

Turbojet · Microturbo

Maximum Takeoff Thrust

1.1 kN

Diameter

325 mm

Length

650 mm

Dry Weight

37 kg

Thrust To Weight

Specific Fuel Consumption

35 g/(kN·s)

Architecture

Fan	Fan Stages —	Fan Blades —	Fan Technology —	Fan Pressure Ratio —
Gearbox	Geared Fan No	Gear —	Reduction Ratio —
LP compressor	Low-Pressure Compressor Stages —	Low-Pressure Compressor Technology —	BP Compressor Pressure Ratio —
IP compressor	Intermediary-Pressure Compressor Stages —	Intermediary-Pressure Compressor Technology —	IP Compressor Pressure Ratio —
HP compressor	High-Pressure Compressor Stages —	High-Pressure Compressor Technology —	HP Compressor Pressure Ratio —
Combustor	Combustion Chamber Folded, with ten spill type burners.
HP turbine	High Pressure Compressor Stages —	High-Pressure Turbine Technology —
IP turbine	Intermediary-Pressure Turbine Stages —	Intermediary-Pressure Turbine Technology —
LP turbine	Low-Pressure Turbine Stages —	Low-Pressure Turbine Technology —
Whole engine	Streams 1	Bypass Ratio —	Overall Pressure Ratio —	Afterburner No

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Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)
Caproni Vizzola Ventura	Microturbo TRS 18	2	6.19	10
NASA AD-1	Microturbo TRS 18	2	11.83	9.85

All data (17 fields)

Name: Microturbo TRS 18
Aircraft Engine Manufacturer: Microturbo
Aircraft Engine Type: Turbojet
Dry Weight (kg): 37
Diameter (mm): 325
Length (mm): 650
Wikipedia Article (URL): en.wikipedia.org/wiki/Microturbo_TRS_18
Fuel: Electric pump.
Geared Fan: No
Combustion Chamber: Folded, with ten spill type burners.
Afterburner: No
Streams: 1
Maximum Takeoff Thrust (kN): 1.1
Thrust To Weight: 3
Specific Fuel Consumption (g/(kN·s)): 35
Compressor Description: Centrifugal; one piece with diffuser and straightener vanes.
Turbine Description: Axial.