CSCA UAV
SSC UAVs are Chinese UAVs developed by Beijing Skyship-Century Aviation and Technology Co., Ltd. (CSCA, 北京中天华航航空科技有限公司), whose UAV products cover fixed and rotary wing aircraft, blimps, and ballons.
SF-GS
SF-GS UAVs are first UAVs developed by CSCA, and they are unmanned blimps that have been deployed in aerial photographic / cinematography missions in the celebration of forty-eighth anniversary of the establishment of the People’s Republic of China, fiftieth anniversary of the Inner Mongolia Autonomous Region, and other events. SF-GS is no longer in production and is succeeded by SSC series unmanned blimps, but some of them are still in service. During its decade long service, SF-GS series unmanned blimps have also been deployed in engineering and industrial missions such as setting up power lines.
SSC unmanned blimps
SSC unmanned blimps are gasoline-powered unmanned blimps developed by CSCA, and they are named after their respective length. For example, if a SSC blimp is 11 meter long, then it is named as SSC-11D. SSC unmanned blimps utilize commercial off-the-shelf (COTS) subsystems such as autopilots and ground controls from MicroPilot.
Model # |
SSC-11D |
SSC-13D |
SSC-GS16D |
SSC-20D |
|---|---|---|---|---|
Length (m) |
11 |
13 |
16 |
20 |
Diameter (m) |
2.5 |
3.1 |
3.8 |
4.5 |
Heigh (m) |
3.3 |
4.3 |
5 |
5.7 |
Volume (m3) |
33 |
52 |
120 |
220 |
Gas |
Helium |
Helium |
Helium |
Helium |
Fuel |
Gasoline |
Gasoline |
Gasoline |
Gasoline |
Max speed (km/hr) |
55 |
60 |
60 |
65 |
Cruise speed (km/hr) |
35 |
40 |
40 |
45 |
Take-off weight (kg) |
37 |
58 |
132 |
235 |
Payload (kg) |
7 |
15 |
30 |
50 |
Endurance (hr) |
2 – 3 |
2 – 4 |
2 – 4 |
2 – 5 |
Normal operating altitude (m) |
≤ 500 |
≤ 500 |
≤ 500 |
≤ 500 |
Remote control radius (km) |
1 |
1 |
1 |
1 |
Power plant |
Komatsu 380-620PU |
Komatsu 800PU |
Komatsu 3W106 |
Komatsu 3W140 |
Ground control |
Horizonmp |
Horizonmp |
Horizonmp |
|
Autopilot |
MP2028 |
MP2028 |
MP2028 |
|
Propeller |
Master |
Master |
Master |
|
SSC unmanned helicopters
SSC unmanned helicopters are two-stroke gasoline-powered unmanned helicopters developed by CSCA, and a total of two have been identified by 2013, the smaller SSC-H260 with fuselage constructed of carbon fiber, and the larger SSC-H800 with fuselage constructed of aluminum – maginesium alloy. SSC unmanned helicopters utilize commercial off-the-shelf (COTS) subsystems such as autopilots and ground controls from MicroPilot. Both unmanned helicopters are equipped with rotors constructed of carbon fiber. H stands for Helicopter.
Model # |
SSC-H260 |
SSC-H800 |
|---|---|---|
Length (m) |
1.75 |
2.146 |
Width (m) |
0.4 |
0.508 |
Heigh (m) |
0.7 |
0.711 |
Fuel |
Gasoline |
Gasoline |
Take-off weight (kg) |
9 |
32.23 |
Payload (kg) |
4 |
12 |
Endurance (min) |
20 |
50 – 55 |
Power plant |
KZ-26 single cylinder |
KZ-80 twin cylinder |
Ground control |
Horizonmp |
|
Autopilot |
MP2128heli |
|
Gyroscope |
Futaba GY611 |
Futaba GY611 |
SSC electrically powered UAVs
SSC electrically powered UAVs are battery powered unmanned UAVs developed by CSCA, and a total of two have been identified by 2013, the smaller SSC-1000EP mini, and the larger SSC-2000EP. SSC electrically powered UAVs utilize COTS subsystems such as autopilots and ground controls from MicroPilot. EP stands Electrically Powered.
Model # |
SSC-1000EP mini |
SSC-2000EP |
|---|---|---|
Wing span (m) |
1.4 |
2.4 |
Chord length (m) |
0.28 |
0.35 |
Wing area (dm2) |
39 |
84 |
Length (m) |
1 |
1.2 |
Take-off weight (kg) |
2.1 |
6 |
Payload (kg) |
0.3 |
0.65 – 1 |
Endurance (hr) |
0.5 |
1.5 |
Range (km) |
70 |
110 |
Ceiling (km) |
3.5 |
4.5 |
Normal operating altitude (m) |
50 – 150 |
100 – 600 |
Power plant |
Battery |
Battery |
Ground control |
Horizonmp |
|
Autopilot |
MP2028 |
|
Launch |
Hand thrown |
Catapult |
Recovery |
Glide |
Parachute |
SSC gasoline-powered UAVs
SSC gasoline-powered UAVs are petrol-powered unmanned UAVs developed by CSCA, and a total of three have been identified by 2013, SSC-GS01, SSC-GS02, and the larger SSC-GS03. SSC gasoline-powered UAVs are constructed of composite material, and SSC-GS03 is an enlarged development of SSC-GS-02. SSC gasoline-powered UAVs utilize COTS subsystems such as autopilots and ground controls from MicroPilot, and Komatsu 3W series engines.
Model # |
SSC-GS01 |
SSC-GS02 |
SSC-GS03 |
|---|---|---|---|
Layout |
Conventional |
Twin boom |
Twin boom |
Wing configuration |
High wing |
Hing wing |
Hing wing |
Empennage |
T-tail |
Twin tail |
Twin tail |
Landing gear |
Tricycle |
Tricycle |
Tricycle |
Wing span (m) |
3.6 |
3.8 |
4.6 |
Length (m) |
2.2 |
2.5 |
3.2 |
Take-off weight (kg) |
23 |
32 |
70 |
Payload (kg) |
5 – 8 |
5 – 10 |
10 – 20 |
Endurance (min) |
2 – 3 |
2 – 4 |
4 – 5 |
Range (km) |
100 |
180 |
250 |
Ceiling (km) |
3.6 |
4 |
4.5 |
Max speed (km/hr) |
130 |
150 |
190 |
Cruise speed (km/hr) |
110 |
130 |
150 |
Power plant |
5 – 6 hp pusher engine |
8 – 10 hp pusher engine |
15 – 20 hp pusher engine |
Propeller |
Two-blade |
Two-blade |
Two-blade |
Fuel |
Gasoline |
Gasoline |
Gasoline |
Ground control |
Horizonmp |
Horizonmp |
|
Autopilot |
MP2028 |
MP2028 |
|
Launch |
Catapult |
Taxiing |
Taxiing |
Recovery |
Parachute |
Taxiing |
Taxiing |
Take-off distance (m) |
50 – 100 |
70 – 120 |
100 – 150 |
Landing distance (m) |
100 – 150 |
100 – 200 |
120 – 200 |
See also
List of unmanned aerial vehicles of the People's Republic of China