Experimental Micro-Rocket Engine for Orbital Manuevering Applcations

Student group is working hard to develop micro sized gaseious Propellant Rocket Engines using Oxygen and Propane for onboard trajectory correction in space.

            
                                                     Static Water test of Centrifugal Injector-1

                                                    Static water Test of the Injector-2

                                                             Injector Head Assembly (a)

Injector head Assembly (b) 

                   

                                                      Single Chamber Injetcor (a)

                                          

Hypersonic Sounding Rocket "Shivastra-1" for Microgravity and X-Ray research

"SHIVASTRA-1" Sounding Rocket on the mobile truck launcher

Apogee achieved 200 km with maximum payload 10 kg

                                                         Upperstage of Shivastra-1 in space

Static Fire of Liquid Rocket Engine At Static Test Stand of  Bharuk Aerospace Ltd.

www.bharuk-as.co.cc

A Micro Liquid Rocket Engine Static Test fire with gaseious propellants Oxygen and Propane 

build for experimental purpose 

Advanced Micro-UAV for Cartography and Monitoring "Sparrow-s"

                            
                                                           "SPARROW-S"
  

Take-off weight	1.2 Kg max
Take-off	Hand Launch

Endurance		30 minute, 45 minute optional
Min. & Max. Ceiling	50 m to 800 m,  3 000 m optional

Payload	Photo with high spatial resolution, nIR, other sensors, more Payload option in big fuselage bay
UAV Lifetime	1 000 flights
Photogrammetry & 3D DSM services	Web solutions for clients  optional

 www.bharuk-as.com                                                                                               www.bharuk-as.co.cc