• Aircraft Wing Structure

    In aeronautics Wing are airfoils attached to each side of the fuselage, So the design of the wing depends on many facts like lift to weight ratio, rate of climb, size, weight and which aircraft it is used,

  • AirCraft Fuselage Structure

    Fuselage is a body of an aircraft to which the wings, tail and Landing Gear units are attached. Design and size of the fuselage varies according to the function to the aircraft. The word fuselage comes from a French word “fusele” means “splindle-shape”

  • Landing Gear

    Landing gear is an undercarriage part of the flight landing system. Aircraft landing gear has wheels equipped with shock absorbers on light planes and Hydraulic or pneumatic oleo struts on larger aircraft.

Showing posts with label Rocket Technology. Show all posts
Showing posts with label Rocket Technology. Show all posts

Sunday, December 6, 2020

Parts of Scramjet Engine

Scramjet Engine

        Scramjet is a variation of a Ramjet Engine, It is a type of Air breathing Engine where the combustion takes place in subsonic airflow, Scramjet  is supersonic throughout the entire engine , Scramjet operate more effective at extreme high speed of about Mach 5.




Parts of Scramjet Engine

  • Inlet
  • Isolator
  • Combustor
  • Nozzle



 

        The different Part of a Scramjet engine is Inlet, Isolator, Combustor and Nozzle. The scramjet engine must be integrated with the Fuselage of the aircraft, specially the air inlet and the Nozzle. Part of the forebody aircraft fuselarge makes the function of air let compressing the freestream air, and the after body acts as a nozzle expanding the gases for the combustion.

Tuesday, December 1, 2020

Salient Features of Liquid Propellant Rockets

  

Salient Features of Liquid Propellant Rockets:


                A liquid propellant propulsion system is commonly called rocket engines. It has all the hardware components and propellants necessary for its operations for producing thrust.



Liquid propellant propulsion system

Consists of one or more thrust chambers, one or more tanks to store propellants, a feed mechanism to force the propellants from the tanks into the thrust chamber, power source to furnish the energy for the feed mechanism, suitable plumbing or piping or piping to transfer the liquids,




Has a structure to transmit the thrust force, and control devices to initiate and regulate the propellant flow and thus the thrust.

In some application an engine may also include a thrust vector control system, various instrumentation and residual propellant (trapped in pipes, valves, or wetting tanks).

It does not include hardware for non-propulsive purpose, such as aerodynamic surface, guidance, or navigation equipment, or useful payload such as scientific space exploration package or missile warhead.