HAPITH V
is a cost-effective space launch system using cutting-edge, non-explosive hybrid rocket technologies. Our hybrid rocket engines are delivering class-I rocket engine performance that enables fast turnaround space launch services.
PAYLOAD
MICRO AND SMALL SATELLITES TO LOW EARTH ORBIT (LEO) AND SUN-SYNCHRONOUS ORBIT (SSO)
HAPITH V OVERVIEW
MAX. LEO PAYLOAD MASS
390 KG
MAX. SSO PAYLOAD MASS
350 KG
ALTITUDE
600 – 700 KM
HEIGHT
20 M
DIAMETER
2.2 M
STAGES
3
UPPER STAGE
single hybrid rocket engine with gimbaled thrust vector control (TVC) and a cold-gas reaction control system (RCS)
THRUST 10KN
SECOND STAGE
cluster of four hybrid rocket engines with gimbaled thrust vector control (TVC)
THRUST 80KN
FIRST STAGE
cluster of five hybrid rocket engines with liquid-injection vector control (LITVC)
THRUST 650KN
P L U G – I N P A Y L O A D > >
C A R B O N C O M P S I T E M A T E R I A L S > >
A V I O N I C S S Y S T E M > >
L E L I E N 1 A H Y B R I D R O C K E T E N G I N E > >