Sets the current isp and mass flow rate. Computes the thrust using the rocket equation. Returns false on an error.
| [Visual Basic .NET] |
|---|
|
| [C#] |
|---|
|
| [Managed C++] |
|---|
|
| [Unmanaged C++] |
|---|
|
| [Java] |
|---|
|
[Python - STK API ] |
|---|
def SetIspAndMassFlowRate(self, Isp:float, MassFlowRate:float) -> bool: |
- Isp
- Must be non-negative.
- MassFlowRate
- Mass loss rate. May be entered as positive or negative number, but is always considered a mass loss, not a mass gain.
Returns false if Isp is negative.
Computes thrust from the rocket equation






