what is the highest temperature the space shuttle undersurface experiences during its mission?
2 10713what are the selected criteria for design of the thermal protection system for the second generation RLV?
2439How difficult is to mould and shape graphite epoxiescompared with alloys or ceramica that may be used for thermal protective applications?
2183why are all shear loads and twisting moments set to zero for the preliminary design phase of TPS?
2672Are thermal protection systems of space crafts commonly composed of one panel or a collection of smaller tiles?
2 5935Does n't simplification of complex honeycomb designed for thermal protection system of areusable launch vehicle jeopardize the accuracy of results?
1 51381.how to sit in a interview(ie. about body language ) 2.why you would like to join the aviation industry. 3.why you selected this company.
AirIndia, Event Management, FlyDubai, Jet Airways, Kingfisher, Manish Pharma, Quest,
18 46127why we use delta connection in primary and star connection in an distribution transformer,which converts 400V a.c voltage to 33KV?
2 5276Post New Aeronautical Engineering Questions
Tell me how would you handle if your co-worker is not co-operating with you?
Explain what will be the responsibility of the spacecraft operations, dynamics and controls?
What are the three tactical elements of electronic warfare?
Discuss the challenges of designing aircraft for different operating environments, such as commercial aviation, military, or space exploration.
How do I decide which is the best technology to solve my vibration isolation problem?
What do you mean by ducting?
What is the use o firewall?
what is the slope angle of the APPROACH LIGHT? and How to calculate it?
Without air traffic control, what is the minimum descent rate you can descend the plane?
Why is the study of gyroscopes motion required to learn aircraft applications?
Tell me about stress analysis?
Discuss the importance of materials selection in aeronautical engineering and how it impacts aircraft performance.
How do you approach the integration of propulsion systems into aircraft design, and what factors influence your decisions?
What will be the responsibility of the spacecraft operations?
How long the oxygen last for passenger in an emergency?