A rocket is fired vertically from the surface of Mars with a speed of `2kms^(-1)`. If `20%` of its initial energy is lost due to Martian atmospheric resistance, how far will the rocket go from the surface of Mars before returning to it? Mass of Mars `=6.4xx10^(23)kg`, radius of Mars `=3395 km`,

A rocket is fired fired vertically from the surface of Mars with a speed of 2 Kms^(-1) . If 20% of its initial energy is lost due to martain atmospheric resistance, how far will the rocket go from the surface of Mars before returning to it ? Mass of Mars= 6.4xx10^(23) Kg, radius of Mars=3395 Km, G= 6.67xx10^(-11)Nm^(2)Kg^(-2) .

A rocket is fired fired vertically from the surface of Mars with a speed of 2 Kms^(-1) . If 20% of its initial energy is lost due to martain atmospheric resistance, how far will the rocket go from the surface of Mars before returning to it ? Mass of Mars= 6.4xx10^(23) Kg, radius of Mars=3395 Km, G= 6.67xx10^(-11)Nm^(2)Kg^(-2) .

A rocket is fired ‘vertically’ from the surface of mars with a speed of 2 km s^-1. If 20% of its initial energy is lost due to martian atmospheric resistance, how far will the rocket go from the surface of mars before returning to it ? Mass of mars = 6.4xx10^23 kg , radius of mars = 3395 km, G = 6.67xx10^-11 N m^2 kg^-2 .

A rocket is fired ‘vertically’ from the surface of mars with a speed of 2 km s^(–1) . If 20% of its initial energy is lost due to martian atmospheric resistance, how far will the rocket go from the surface of mars before returning to it ? Mass of mars = 6.4 xx 10^(23) kg, radius of mars = 3395 km, G = 6.67 xx 10^(-11) N m^(2) Kg^(-2) .

A rocket is fired ‘vertically’ from the surface of mars with a speed of 2 km s^(–1) . If 20% of its initial energy is lost due to martian atmospheric resistance, how far will the rocket go from the surface of mars before returning to it ? Mass of mars = 6.4 ×x 10^(23) kg, radius of mars = 3395 km, G = 6.67 xx 10^(-11) N m^(2) Kg^(-2) .

A rocket is fired vertically from the surface of mars with a speed of 2 km/s. If 20% of its initial energy is lost due to martian atmosphere resistance how far (in km) will the rocket go from the surface of mars before returning to it? Mass of mars =6.4xx10^(23) kg, radius of mars =3395 km, G=6.67xx10^(-11)Nm^(2)//kg^(2) .

A rocket is fired vertically from the surface of 2kms^(-1) . If 20% of its internal energy is lost due to the Martian atmospheric resistance , how far will the rocket go from the surface of Mars before returning back ? Mass of Mars = 6.4 xx10^(24)kg, radius of Mars = 3395 km , G = 6.67xx10^(-11) Nm^(2) kg^(-2)

A rocket of mass m is field vertically from the surface of Mars of mass M , radius R with a sped upsilon . If 20% of its initial energy is lost due to Martain atmosheric resistance, how far will the rocket go from the surface of Mars before returing to it? Let G be the gravational constant.