Moreover on the wings and fuselage of the craft. Need very strong,durable,and also temperature resistance to any radical changes that may occur and effect any structural strength of the wings.(Hot or cold ). Also it shall b constructed for glider use at high alt. May install system for any emg.bail out or eng. failures that may occur. Nd any imput as to what internet address I can contact 4 any further info.
Answer:
FYI:
Ultralight aircraft are under 500 lb.s max gross weight.
(Thats you, engine, fuel, plus the airframe.) - No allowance for "emg. bail out". If you've got an engine failure you glide it down.
This means precise design is critical to get enough strength and power into the same package even to take off. - NOT an amateur activity.
They are restricted to low altitude.
No high altitude gliding except by special clearances.
This project is way beyond your skill level if you have to ask those questions..
The answers post by the user, for information only, FunQA.com does not guarantee the right.
More Questions and Answers:
Could solar panels be put in hot parking lots to convert the heat generated from the pavement?
Is going back to get a civil engineering degree the right choice?
I need help deciding on college courses! Electrical Eng or Computer Information?
I am Electrical and Electronics Engineer, 35 yeard experience and 54 years old. How to get a job in Canada?
Is it possible for a flight (passenger or watever) to stop on air?
If I have a bearing from certain vendor example caterpillar with which vendor can i relace its bearing?
What is a pre-pop test for a safety relief device?
What size particles do hay bales filter?
Advantages and disadvantages of DC source?