Antrik - 1 is a Modular Small Satellite Launch Vehicle.
Capable of taking upto 300 kg to orbits around 500 km high, Antrik - 1 can take payload to low and high inclination orbits. Designed with resusability in mind hence it can return to land. It uses LOX/CH4 based engines in all its stages and Antrik - 1 is configurable to the mission needs of the customer. It uses Advanced propulsion, materials and Purposely designed flight profile to any specific mission.
Facts & Figures
Second Stage(5.3m & 17.4ft)
second stage engine
lightning 2
qty engines :1
propellant
thrust:163 KN (36,643 ibf) (VAC)
isp: 324.0 seconds (VAC)
Second stage avionics
flight computer
multi-band path array antennae
GPS/IMU navigation
power conditioning & distribution unit (PCDU)
solenold drive , telemetry transmitter
data acqusition chassis (DAC)
lithium polymer batteries
autonomous flight termination system
payload segment(6.5m 21.3ft)
payload
300kg LEO 28.5*, 500km
primary payload
payload farining
carbon composite structure
1.6m (9.2 ft) diameter
18m2(798.1 ft) of internal volume
(primary payload)
#aero2astro
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