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keywords - Re-entry Vehicles, Wiedereintritt, Landekapsel, Ρalculation, Berechnung, Wostok, Sojuz, Apollo, Space Shuttle, Meterorit, Luna, Superlight Reentry Vehicles
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| Models | Example |
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Wostok ( K = 0 V
= 7,8 km/s ) Sojuz ( K = 0,25 V = 7,8 km/s ) Apollo ( K = 0,3 V=11,2 km/s ) Space Shuttle ( K = 1,4 V= 8 km/s ) Meterorit ( K = 0, V = 20 km/s, Density=2t/m3, D=10m) Luna-16 ( K = 0, V = 11,2 km/s ) Superlight Reentry Vehicles ( K = 0 V = 7,8 km/s) Superlight Reentry Vehicles ( K = 0,3 V = 7,8 km/s) Apollo ( K = 0,0 V=11,2 km/s ) - ballistic Re-Entry |
Example 1 - Sojuz ( K = 0,25 V = 7,8 km/s )
Example 2 - Apollo ( K = 0,3 V=11,2 km/s )
Meterorit ( K = 0, V = 20 km/s, Density=2t/m3, D=10m)
Superlight Reentry Vehicles ( K = 0,3 V = 7,8 km/s)
