To initiate reentry a retrofire is used to slow the spacecraft and drop into atmosphere Friction with atmospheric molecules produces extreme heat A blunt.

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Presentation transcript:

To initiate reentry a retrofire is used to slow the spacecraft and drop into atmosphere Friction with atmospheric molecules produces extreme heat A blunt surface is best on the front of the spacecraft. This will produce a shock wave in front to absorb heat Materials on the outer surface to protect the spacecraft have varied. Early spacecraft such as those used in the Mercury, Gemini and Apollo programs used ablation - where the surface vaporises and takes heat away The space shuttle uses insulating tiles which provide a protective barrier that prevents heat entry Another issue is g-forces: A deceleration of near 3g is preferable, higher g-forces cause discomfort and affect body function - 8g may cause chest pain, loss of consciousness g-forces: a transverse (front to back) application is best, as up or down forces can cause too much or too little blood to the brain g-forces: eyeballs in! g-forces: contoured body support Ionisation blackout: heat causes layer of ionised particles preventing radio contact for some minutes Landing: After re-entry, parachute to water for earlier missions so flotation of capsule and location are important; Shuttle: banked turns and controlled descent to runway Discuss issues associated with safe re-entry into the Earth’s atmosphere and landing on the Earth’s surface

The optimum angle of re-entry is best angle for the spacecraft to approach the level of the atmosphere If the angle is too steep, the spacecraft will collide with too many atmospheric molecules too quickly at high speed, causing the temperature to rise dramatically and causing the spacecraft to burn up. The g-forces would also be too great, causing loss of consciousness or fatality. By ensuring the correct time, direction and duration of the retroburn (forward facing rockets) If the angle is too shallow the spacecraft will not re-enter, but ‘skip’ off the atmosphere For the Apollo spacecraft, the optimum angle was between 5.2 and 7.2 degrees below horizontal What is meant by optimum angle of re-entry? What is an example of an optimum angle of re-entry? How is the correct angle achieved? What are the consequences of failing to achieve this angle?