Select Rocket:
Calculated Attributes
| Source | Total Mass | Mass No Motor | Length | Max Diameter | CG | CP | Stability (cal) |
|---|---|---|---|---|---|---|---|
| RW | --- |
--- |
--- |
--- |
--- |
--- |
--- |
| OR | --- |
--- |
--- |
--- |
--- |
--- |
--- |
Components
Choose Motor:
Motor Specs
| Name | Case | Length | Total Impulse (I) | Avg Thrust (T) | Max Thrust (T_MX) | Burn Time | Total Mass | Prop Mass | Empty Mass | Prop Type | Delay |
|---|---|---|---|---|---|---|---|---|---|---|---|
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
Thrust Curve
| Select Algorithm | Compare to | ||
| Max Sim Time (s) | |||
| Frame Size (s) 'dt' | |||
| Frame Rate (ms) | |||
| Mach 'M' | |||
| Rod Length |
| System | Configuration | Objective | Desired Value | Action |
|---|---|---|---|---|
| Aero Brakes | Altitude | (m) |
Frame Rate : ---ms Step(dt) : ---s
Telemetry
| Time (s) | Thrust (N/s) | Weight | Drag | Net | Alt (m) | v (m/s) | a (m/s^2) | Cd |
|---|
Aerobrakes
| Time (s) | Alt (m) | v (m/s) | Apg_p (m) | Error (m) | Angle° | Cd_adj | D_apogee/d_angle | Auth | Alt_noise | v_noise | Achievability |
|---|
Flight Events
| Event | Time (s) | Thrust (N/s) | Weight | Drag | Net | Alt (m) | Velocity (m/s) | Acceleration (a) | Cd |
|---|
Simulation Comparisons
NOTE: Number inside "()" is the % a particular value deviates from OpenRocket's calculated number. Color indicates severity of deviation
| Source | Configuration | Velocity off rod | Apogee | Velocity at Deployment | Opt Delay (t_coast) | Max. velocity | Max. accelleration | Time to apogee | Flight Time | Ground hit (vert only) |
|---|---|---|---|---|---|---|---|---|---|---|
| RK4 (1DOF) | --- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
| Euler (1DOF) | --- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
| Closed Form (1DOF) | --- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
| OpenRocket (RK4-6DOF) | --- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |
--- |