|
|
|
|
|
|
|
|
|
|
|
|
||||
|
|
|
|
|
|||
|
|
||||||
|
|
||||||
|
Many of the conclusions published in the
book "Astronautical Engineering" are
based on numerical results of the following software products:
1. Space Launcher Trajectory
Optimization 2. Launch Vehicle System Analysis 3. Reentry Trajectory Simulation 4. Space Launcher Navigation 5. Planetary Mission Design
The example above shows the printout of
a reference trajectory for a study of the European Ariane-5 launcher
during the preliminary design phase.
1. Normal Force Coefficient and its
Derivative 2. Pitching Moment Coefficient and its
Derivative 3. Center of Pressure Location and its
Static Margin
The example above shows the printout
of aerodynamic performance data for the feasibility study of a small
airborne launcher derived from Ariane-4
components. |
|
|
||||
|
|
||||||
|
|||||||
|
|