Name
|
Description
|
Attributes
|
AttitudeSystem
|
Flag denoting the attitude frame in which the thrust event will be applied to the spacecraft.
|
Type: Variable
Access: Read/Write
|
BurnDirection
|
The components of the thrust vector in the coordinates of the attitude system specified by the chosen AttitudeSystem.
|
Type: Array
Access: Read/Write
Units: km/s^2
|
DeclaredName
|
The name of the object as declared.
|
Type: String
Access: Read-Only
|
DisplayName
|
The name displayed for this object in output windows such as views, plots, and reports.
|
Type: String
Access: Read/Write
|
EventDuration
|
The duration of the outgassing event. This is determined based on the TimeConstant and the MinimumMagnitude properties.
|
Type: TimeSpan
Access: Read-Only
Units: day
|
EventStartTime
|
The offset time from current Spacecraft epoch, to apply the outgassing event. The Spacecraft will be propagated to the offset time using the applicable ForceModel and Propagator properties. A negative offset time can be used.
|
Type: TimeSpan
Access: Read/Write
Units: s
|
ExecutionPhase
|
Reveals which portion of the event sequence is currently executing.
|
Type: Variable
Access: Read-Only
|
MinimumMagnitude
|
The cut-off threshold for modeling the exponentially decaying outgassing event.
|
Type: Variable
Access: Read/Write
|
ObjectId
|
The unique identifier for the object.
|
Type: Variable
Access: Read-Only
|
ObjectType
|
The type of the object.
|
Type: String
Access: Read-Only
|
OD
|
This property contains the OD settings for all the OutgassingEvent properties that can be estimated.
|
Type: OutgassingEventODProperties
Access: Read-Only
|
TimeConstant
|
The time constant of the exponential decay function that is used to model the outgassing event.
|
Type: Variable
Access: Read/Write
Units: s
|
