# objectives
>investigate the atmosphere and magnetoshere of Jupiter
>invesigate the surfacce of Io

# instruments

mass mostly necessary for inertia matrix

## atmosphere and surface spectrometer

### stats
$3.1kg$
$6.7W$
$195 \times 205 \times 310 mm$

## dual imaging system

### stats
$8.0kg$
$7.6W$
$260\times 560 \times 630 mm$

## magnetometer

### stats
$4.4kg$
$4.2W$
sensor: $81\times 48 \times 46 mm$
electronics: $130 \times 104 \times 86 mm$
boom: $3600 mm$

## particle and plasma spectrometer

### stats
$3.1 kg$
$7.8W$
$185\times 205 \times320 mm$

# burns to calculate

all orbits are coplanar

## distance between earth and jupiter at the transfer
## time between earth and jupiter
## $\Delta V$ and propellent mass for jupiter insertion
## burn duration for jupiter insertion
## $\Delta V$ and propellent mass for Io intercept
## $\Delta V$ and propellent mass for disposal orbit
## minimum propellent mass

# spacecraft numbers
dry mass: $550kg$
## primary propulsion
mass: $3.78 kg$
power: $37W$
thrust: $400N$
specific impulse: $320s$