Mini Airship

 

Micro Airship

 

Flight Trials at Pune, 28 - 30 December 2002

 

  Demonstration of a Remotely Controlled Airship at 90'th Indian Science Congress

 

 

Mini Airship

 

During the conceptual design phase of PADD, an unmanned scaled down prototype of the PaxCargo airship, named as Mini airship was developed by PADD project team. The aim of design and fabrication of this prototype was to explore the possible use of remotely controlled airship as an ideal mean for aerial surveillance. Mini airship was demonstrated successfully during the 90th Indian Science Congress held in January 2003 which was witnessed by the respected president Dr. A P J Abdul Kalam, former ISRO chairman, Dr. K. Kasturirangan and many respected officers from Indian army, and citizens.

 

*    Remotely controlled with a Four Channel receiver operated by a FM Transmitter

*    Length 6.7 m (22 ft) with fineness ratio 4

*    Envelope volume 8.6 m3

*    Payload capacity 3 kg

*    Powered by 7.5 cc IC engine which produces 1.65 HP

*    Max. speed achieved 36 kmph at 200 ft.

*    Endurance 15 minutes with 250 ml fuel

*    Fitted with onboard Video Downlink system to transmit real time video to ground station

*      So far, Mini airship has been test flown at Pune Gliding Centre (Dec. 2002), Bangalore University Campus (Jan 2003) and recently at Park College of Engineering, Coimbatore (Sept. 2004)

 

                     

                                                        

        Attachments and Inspections

        Getting out of Hanger

        Pre Flight Inspections

        Just Took off

        Over the Hanger

        Deep in the sky

        Look at the range

        Lets land now

        What a safe Landing !!!

 

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Micro Airship

 

With a view to get a first hand exposure to the issues related to designing and operating airships, a team of project engineers designed, fabricated and flight tested a remotely controlled airship later called as Micro airship.

This activity was seamlessly integrated with the Aircraft Design Laboratory course for the undergraduate students of the Aerospace Engineering Department, enabling them to participate in a live aircraft design project from the conceptualization to realization.

 

 

*      Remotely controlled with a Four Channel receiver operated by a FM Transmitter

*      Length 5 m (16.4 ft) with fineness ratio of 3.05

*      Envelope volume of 6.8 m3

*      Payload capacity of ~ 1 kg

*      Powered by  one 2.5 cc IC engine which produces 0.40 HP

*      Max. speed achieved 25 kmph at 200 ft.

*      Endurance 15 minutes with

200 ml fuel

 

        Gondola and final attachment

        Shifting to the Ground

        Ready to take off

        Just Took off

        Here she goes!

        Aerial wonder !!!

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