Consultancy

Hybrid Rocket Motor Test Facility

The hybrid rocket facility can cater testing of a laboratory scale hybrid rocket motor with various solid fuel and oxidizer compositions. The below mentioned facilities are open for students/research scholars from other institutions at a nominal charge. For more details contact: Dr. Sri Nithya Mahottamananda.

Hybrid rocket motor has got good advantages over solid rocket motor and liquid rocket engines in various mission requirements such as reignition capability, modulation of thrust, minimum environmental effect, and improved safety – which make it suitable for a broad range of applications including sounding rocket, tactical missile, launch vehicle propulsion and space exploration etc.

Hybrid Rocket Motor

Static Test Firing

GOX Feed line setup

Ballistic test control unit and data acquisition facility

Propellant Mixer with Hot water Bath

Vacuum Pump – Propellant Casting Unit

Propellant Curing Oven (Electric Type) (500 x500x500 mm)

Fuel grain

• REQUEST FORM – HYBRID ROCKET BALLISTIC TEST

For more details please contact:

Head of the department,
Department of Aerospace Engineering,
Email:hod@crescent.education
Ph: +914422759241