ContinuousThrustForceModelCreateVeThrustVector Method

Creates a thrust Vector where the thrust is computed from the exhaustSpeed, and massFlowRate pointing in the thrustDirection in the specified burnAxes.

Namespace: AGI.Foundation.Celestial
Assembly: AGI.Foundation.OrbitPropagation (in AGI.Foundation.OrbitPropagation.dll) Version: 24.2.419.0 (24.2.419.0)

Syntax

C++

Copy

public static Vector CreateVeThrustVector(
	Scalar exhaustSpeed,
	Scalar massFlowRate,
	Axes burnAxes,
	Vector thrustDirection
)

Public Shared Function CreateVeThrustVector ( 
	exhaustSpeed As Scalar,
	massFlowRate As Scalar,
	burnAxes As Axes,
	thrustDirection As Vector
) As Vector

public:
static Vector^ CreateVeThrustVector(
	Scalar^ exhaustSpeed, 
	Scalar^ massFlowRate, 
	Axes^ burnAxes, 
	Vector^ thrustDirection
)

static member CreateVeThrustVector : 
        exhaustSpeed : Scalar * 
        massFlowRate : Scalar * 
        burnAxes : Axes * 
        thrustDirection : Vector -> Vector

Parameters

exhaustSpeed: Type: AGI.Foundation.GeometryScalar
The speed of the exhaust.
massFlowRate: Type: AGI.Foundation.GeometryScalar
The fuel flow rate.
burnAxes: Type: AGI.Foundation.GeometryAxes
The axes to compute the thrustDirection in.
thrustDirection: Type: AGI.Foundation.GeometryVector
The direction of the thrust in the burnAxes.

Return Value

Type: Vector
A vector representing the thrust.

Reference

ContinuousThrustForceModel Class

AGI.Foundation.Celestial Namespace

ContinuousThrustForceModelAddLanguageSpecificTextSet("LSTFD1DBFEF_0?cpp=::|nu=.");CreateVeThrustVector Method

Parameters

Return Value

Reference

ContinuousThrustForceModelCreateVeThrustVector Method