High Thrust-to-Weight Ratio Turbojet Engine with High-Altitude Rapid Start Capability and 100~300kgf Range for Missiles

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Price: Negotiable

MOQ: Negotiable

Delivery Time: Negotiable

Product Description

High Thrust-to-Weight Ratio Turbojet Engine

Product Advantages

Comprehensive product range (100~300kgf turbojet engines, 400~1000kW turbogenerator engines, and 300~1000kg turbofan engines)
Cutting-edge performance (thrust-to-weight ratio of 10 and high-altitude rapid start capability)
Exceptional stability and reliability (fully validated through 100 test prototypes, high-altitude tests, and flight tests)
High production capacity (annual output of thousands of units)
Excellent after-sales service (professional after-sales support team)
Strong product customization capabilities (customized products deliverable within 3 to 5 months)

Core Products

Product Specifications (Series 1)

Parameter/Model	LJ40P	LJ80P	LJ120P	LJ160P
Power Generation Output (kW)	/	1.6	2	2
Specific Fuel Consumption (kg/(kgf·h))	1.4	1.3	1.2	1.18
Diameter * Length (mm*mm)	156*397	200*482	239*617	275*648
Weight (kg)	4.5	7.8	13.5	20.5
Maximum Take-off Altitude (m)	5000	8000	8000	8000
Maximum Flight Altitude (m)	8000	12000	12000	12000
Maximum Flight Speed (Ma)	0.8	0.95	0.95	0.95

Product Specifications (Series 2)

Parameter/Model	LJ200P	LJ260P	LJ300P
Power Generation Output (kW)	2	2.5	2.5
Specific Fuel Consumption (kg/(kgf·h))	1.15	1.12	1.1
Diameter * Length (mm*mm)	303*726	335*765	350*855
Weight (kg)	30	43	54
Maximum Take-off Altitude (m)	8000	8000	8000
Maximum Flight Altitude (m)	16000	16000	16000
Maximum Flight Speed (Ma)	0.95	0.95	0.95