Impact Averted
Deflection Shift (Δv) 2.74 mm/s
B-Plane Miss Distance 38,420 km
Miss in Earth Radii (R⊕) 6.03 R⊕
Unmitigated Impact Energy 48.2 MT
Mission Time: T - 3.2 Yrs
Impactor Separation: Intercept In-Flight
Deflection Angle (θ): 0.082 mrad
Earth Orbit (1.0 AU)
Unmitigated Trajectory
Deflected Trajectory
Kinetic Impact Point

Planetary Defense Physics & Impact Assessment

Target: Dimorphos analogue | Critical Clearance Achieved
Physical Parameter Target Asteroid Kinetic Impactor Slate Encounter Mitigation Outcome
Mass & Velocity 4.08 × 10⁹ kg 610 kg @ 6.60 km/s +2.74 mm/s along-track
Momentum Boost (β) 2.14 × 10⁶ m³ 1.45 × 10⁷ kg·m/s (β=3.6) 432 km / yr drift rate
Earth Encounter Node 5.0 Years Pre-Impact 6.03 R⊕ cleared SAFE MISS: 38,420 km

Kinetic Impactor Mechanics: Why DART Tested β

When NASA's Double Asteroid Redirection Test (DART) crashed into Dimorphos on September 26, 2022, it did not rely on pure momentum transfer ($m v$). The hypervelocity collision blasted thousands of metric tons of shattered rock and debris backward into space.

This ejecta recoil acts like a miniature rocket engine, multiplying the asteroid's velocity shift by the momentum enhancement factor $\beta$. DART verified $\beta \approx 3.6$, proving that rubble pile asteroids can be deflected more than three times more effectively than solid metal monoliths.

The Geometry of Early Warning & The B-Plane

A millimeter-per-second velocity change ($\Delta v \approx 2\text{ mm/s}$) applied 10 years before encounter results in tens of thousands of kilometers of along-track orbital displacement at the Earth intersection node.

In the target B-plane coordinate system, Earth's capture radius is expanded by its gravitational focus: $b_{crit} = R_{\oplus}\sqrt{1 + (v_{esc}/v_{\infty})^2}$. Clearing this gravitational focusing boundary guarantees safe passage with zero risk of atmospheric entry or destructive airburst.

Enjoy this tool? Build your own with Super