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Aero Stability (CoP)

AERO STABILITY

STABILITY MARGIN
0.00

CALIBERS (UNITLESS)

FLIGHT STATUS:

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Aero-Stable

The Straight Arrow. Stability is about Passive Recovery. If the Center of Pressure is too far forward, the rocket becomes an "unguided missile" that wants to tumble.

  • 📐 Static Margin: The distance between CG and CP.
  • 🦈 Fins: Used to move the CP further back.
  • 🌪️ Damping: How fast the wobbling stops after a gust.
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AERO-VECTOR SCAN
STABLE SYNC
RESTORE TORQUE: ✅ ACTIVE
AERO-SYNC ACTIVE ✅

Stability Oat

Self-Correcting Geometry. Aerodynamic stability ensures that the atmosphere works with you, not against you, by using the wind to maintain your vector.

  • 🏹 Arrow Effect: Keeping the drag behind the weight.
  • 📈 Alpha Angle: The angle between where you point and where you move.
  • 🛡️ Passive Safety: No computers needed for a stable shape.
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CG
CP
AERODYNAMIC SCAN
MARGIN: 2.5 cal
RECOVERY: ✅ STABLE
STABILITY-SYNC ACTIVE ✅

Vector CG

The Anchor Point. Center of Gravity is the Structural Soul of the vehicle. It dictates how the rocket responds to steering and where it naturally wants to pivot.

  • ⚖️ Equilibrium: The point where all forces sum to zero.
  • 🔄 Rotation: The center of every tumble and turn.
  • Dynamic: CG shifts as the mass "diet" continues.
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MASS DISTRIBUTION
COORD: X-0.4
AXIS: ✅ CENTERED
BALANCE-SYNC ACTIVE ✅

Vector CP

The Force Resultant. Center of Pressure is the Balance of the Wind. It is the invisible hand that tries to flip your rocket if it isn't properly placed behind the CG.

  • 🦈 Fins: The primary tool used to "pull" the CP toward the tail.
  • 📈 Aerodynamics: Purely a function of shape and air flow.
  • 🏁 Trailing: CP must always follow the CG for stability.
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AERO-PRESSURE SCAN
CP: TAIL-SEC
PRESSURE CENTER: ✅ NOMINAL
PRESSURE-SYNC ACTIVE ✅

Balance Fail

The Pivot War. When CP and CG aren't aligned within the "Stability Margin," the aerodynamic forces overwhelm the mass. You lose the Vector of Intent.

  • 🔄 Tumbling: Caused by "Nose-Heavy" pressure.
  • 🌬️ Veering: Caused by "Tail-Heavy" pressure.
  • 🚨 Critical: The rocket follows the wind, not the pilot.
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⚠ STABILITY LOSS
TORQUE ANALYSIS
CP > CG
RESULT: 🔄 UNCONTROLLED PITCH
SAFETY-SYNC FAILED ❌