KZ-1A

KZ-1A three-stage solid launch vehicle is capable of launching and networking multi microsatellites by a single launch using vehicular mobile launch technology. 
KZ-1A launched two satellites into pre-selected orbit in 2013 and 2014 respectively.



KZ-1A Φ1.4m Fairing
PARAMETER
Character
Max.diameter:1.4m
Lift-off mass:30t
Fairing:Φ1.2m/Φ1.4m
Carrying capacity
200kg/700km SSO
Typical Orbit Accuracy: 
Semi-major axis: ≤ 5km 
Inclination: ≤ 0.1° 
Eccentricity: ≤ 0.002
3-Axis Pointing Accuracy:
Angle: ≤ 1° 
Rate: ≤ 0.3°/s
FAIRING
PROPULSION CONTROL MODULE
THIRD STAGE ENGINE
SECOND STAGE ENGING
FIRST STAGE ENGING
TAIL SECTION
GRID RUDDER

Figure 1 Carrying capability launches from Jiuquan Satellite Launch Center

Figure 2 Carrying capability launches from Xichang Satellite Launch Center

Figure 3 Carrying capability launches from Wenchang Spacecraft Launch Center

Figure 4 Carrying capability launches from Taiyuan Satellite Launch Center