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originally posted by: Zaphod58
a reply to: Urantia1111
NASA has used rockets and airbags to land probes. The rocket fires a certain distance off the ground to slow it more, and the airbags deploy around the entire probe and cushion the impact. The parachute is the initial slowing device.
The parachutes that we currently use are designed to slow down the entry vehicle only after they have already lost most of their kinetic energy using a heat shield. However, it you were to design an incredibly large incredibly lightweight parachute and figure out a way to open it up in space before you entered the atmosphere, then it just might be possible to use it to do the job of slowing you down from orbital speed and eliminate the heat shield. The deceleration would occur much higher in the atmosphere where the air is even closer to a vacuum that where current heat shields operate. It turns out that due to the exponential decrease in density with altitude, the decelerate would be essentially the same for any ballistic coefficient. So this hypothetical parachute would still experience about 10 g's of deceleration. But because it would happen in lower density air, the dynamic pressure would be lower and so would the heating rate (W/cm^2). The problem is make this incredibly large and incredibly thin parachute take the deceleration loads.
originally posted by: Chadwickus
a reply to: Urantia1111
I never mentioned airbags.
Boosters are used for the final touch down for a soft landing.
And will most likely be the method (including a parachute) for landing people on Mars