Struct RocketSample 

pub struct RocketSample {
    pub mass_kg: f64,
    pub motor: MotorSample,
}

Motor output and total current vehicle mass.

For a staged vehicle the motor fields are aggregates over every attached motor: summed thrust, summed remaining propellant and a combined phase (Burning if any attached motor burns, else AwaitingIgnition if any is still scheduled, else BurnedOut if any motor existed, else Unpowered).

Fields

mass_kg: f64

Base mass plus attached stage dry mass and remaining propellant, in kilograms.

motor: MotorSample

Aggregated motor output across attached stages.

Trait Implementations

impl Clone for RocketSample

fn clone(&self) -> Self

Returns a duplicate of the value.

fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source.

impl Copy for RocketSample

impl Debug for RocketSample

fn fmt(&self, f: &mut Formatter<'_>) -> Result

Formats the value using the given formatter.

impl PartialEq for RocketSample

fn eq(&self, other: &Self) -> bool

Equality operator ==.

fn ne(&self, other: &Rhs) -> bool

Inequality operator !=.

impl StructuralPartialEq for RocketSample