9. For the same remote-sensing spacecraft to Mars discussed in the previous question.

^{Find v_Mars(Submit your answer as a number which will be assumed to be in km/sec)}

Here's the infogivenwiththe previousproblem:

Earth parking orbit altitude = 1000 km Mars Parking orbit altitude = 500 km_Earth=3.99x10⁵km³/s²_Mars=4.280x10⁴km³/s²_Sun=1.33x10¹¹km³/s²Earth's orbital radius = 1.50 x 10⁸ km (assume earth has a circular orbit for this problem)Mars' orbitalradius=2.28x10⁸km (assume Mars has a circular orbit for this problem)

10. What is the needed phase angle for the rendezvous of a flight from Earth to Jupiter?

Given:

R_toEarth= 1.496 10⁸kmR_toJupiter=7.79 10⁸km

11. For the same remote-sensing spacecraft NASA is sendingto Mars.

Find v_Earth (Submit your answer as a number which will be assumed to be in km/sec)

Here's the infogivenwiththe previousproblem:

Earth parking orbit altitude = 1000 km Mars Parking orbit altitude = 500 km_Earth=3.99x10⁵km³/s²_Mars=4.280x10⁴km³/s²_Sun=1.33x10¹¹km³/s²Earth's orbital radius = 1.50 x 10⁸ km (assume earth has a circular orbit for this problem)Mars' orbitalradius=2.28x10⁸km (assume Mars has a circular orbit for this problem)

12. For the same remote-sensing spacecraft to Mars discussed in the previous question.

^{FindV_boost(Submit your answer as a number which will be assumed to be in km/sec)}

Here's the infogivenwiththe previousproblem:

Earth parking orbit altitude = 1000 km Mars Parking orbit altitude = 500 km_Earth=3.99x10⁵km³/s²_Mars=4.280x10⁴km³/s²_Sun=1.33x10¹¹km³/s²Earth's orbital radius = 1.50 x 10⁸ km (assume earth has a circular orbit for this problem)Mars' orbitalradius=2.28x10⁸km (assume Mars has a circular orbit for this problem)

13. For the same remote-sensing spacecraft to Mars discussed in the previous question.

^{Find V_mission(Submit your answer as a number which will be assumed to be in km/sec)}

Here's the infogivenwiththe previousproblem:

Earth parking orbit altitude = 1000 km Mars Parking orbit altitude = 500 km_Earth=3.99x10⁵km³/s²_Mars=4.280x10⁴km³/s²_Sun=1.33x10¹¹km³/s²Earth's orbital radius = 1.50 x 10⁸ km (assume earth has a circular orbit for this problem)Mars' orbitalradius=2.28x10⁸km (assume Mars has a circular orbit for this problem)

14. For the same remote-sensing spacecraft to Mars discussed in the previous question.

^{Find _Vretro(Submit your answer as a number which will be assumed to be in km/sec)}

Here's the infogivenwiththe previousproblem:

Earth parking orbit altitude = 1000 km Mars Parking orbit altitude = 500 km_Earth=3.99x10⁵km³/s²_Mars=4.280x10⁴km³/s²_Sun=1.33x10¹¹km³/s²Earth's orbital radius = 1.50 x 10⁸ km (assume earth has a circular orbit for this problem)Mars' orbitalradius=2.28x10⁸km (assume Mars has a circular orbit for this problem)