Jumeirah Industry Co.，Limited
Products
Manufacturer of a wide range of products which include China's Leading SAR Satellite Constellation with 0.02° Pointing Accuracy 540W,Turbine Electric Engine with Hybrid Propulsion System - High Efficiency, Low Operating Costs, an...
MOQ:
Price:
| Pointing accuracy | <0.02°,<0.002°/s |
| Accommodation space for payloads | ≥10kg ≥50kg ≥150kg |
| Power alocation for payloads | 540W@15min 3000w @ 3 min |
| X-Band | 100-600Mbps |
| Payload accommodation space | ≥10kg, ≥50kg, ≥150kg |
| Payload power allocation | 540W@15min, 3000W@3min |
| X-Band data rate | 100-600Mbps |
| Payload capacity range | TY20kg to TY300kg |
| Imaging capability | millimeter-level deformation monitoring |
| Model Number | SAR satellite |
| Place of Origin | China |
MOQ: 2
Price: USD： 285000
| Payment Terms | T/T |
| Supply Ability | 100 |
| Power output | 400-1300kw |
| Overall pressure ratio | 8 |
| Turbine inlet temperature(℃) | 1000 |
| Thrust-Specific fuel consumption(kg/kW/h) | 0.44 |
| Weight(kg) | 120 |
| Dimensions(Length×Width ×Height)mm | 1050*520*480 |
| Rated speed(rpm) 57000 | 57000 |
| Power output(kW) | Maximum Continuous 300,Peak 350 |
| Pressure ratio | 8 |
| Inlet temperature | 1000℃ |
| Fuel consumption | 0.44 kg/kW/h |
| Weight | 120 kg |
| Dimensions | 1050×520×480 mm |
| Rated speed | 57000 rpm |
| Max power | 350 kW |
| Range | 1000 km |
| Model Number | CTG400，CTG1000，CTG1600 |
| Place of Origin | China |
MOQ: 2
Price: USD： 410，000-USD-860,000
| Payment Terms | T/T |
| Supply Ability | 200 |
| Delivery Time | 180days |
| Output Shaft Power | 600-kw---1300kw |
| Overall Pressure Ratio | 8.8--13.5 (kg/kW·h) |
| Specific Fuel Consumption | ≥ 0.35---≥ 0.29 |
| Output Shaft Speed | 2000 rpm |
| Weight | 185(Engine Core)+60(Propeller)kg----293kg |
| Engine Core Weight | 185 kg |
| Propeller Weight | 60 kg |
| Total Weight | 293 kg |
| Model Number | GTP 800，GTP 1600 |
| Place of Origin | China |
MOQ: 2
Price: USD :1250000
| Payment Terms | T/T |
| Supply Ability | 20 |
| Delivery Time | 200 Days |
| Takeoff Thrust | 3000 kgf |
| Tota Pressure Ratio | 21 |
| Takeoff Specific Fuel Consumption | (kg/kgf.h)0.42 |
| Core Engine Rotational Speed | 29000 rpm |
| Weight | 480 kg |
| Takeoff Fuel Consumption | 0.42 kg/kgf.h |
| Bypass Ratio | Medium |
| Model Number | TF30 |
| Place of Origin | China |
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