SPECIFICATIONS

Basic configuration	Solid fuel three-stage and liquid propellant upper stage (PBS)
Height	Approximately 18 meters
Total weight	Approximately 23 metric-tons
Diameter	1.35 meters (fairing diameter 1.5 meters)
Launch capability	Sun-synchronous orbit (SSO): 150 kg (inclination 97 degrees, altitude 500 km) Low Earth orbit (LEO): 250 kg (inclination 33 degrees, altitude 500 km)

Launch Vehicle

FAIRING