NEO Deflection App

Time of Deflection (D):

Transfer Time (L to D):

Vehicle:

# Launches:

Vehicle:

# Launches:

Vehicle:

# Launches:

Specify Num Lambert Revs

Mass Delivered to Object:

Simulated Near Earth Object (NEO)

View Orbital
Parameters

Object parameters
are only applicable in
Intercept Mode

Advanced Mode

Tips

Orbit Changes

ΔVA: ... ^mm⁄_s

ΔVC: ... ^mm⁄_s

ΔVN: ... ^mm⁄_s

Total ΔV: ... ^mm⁄_s

Period at D: ... d

Δ Period: ... s

B-Plane Values

ζ (zeta): ... R_e

ξ (xi): ... R_e

B magnitude: ... R_e

Capture Rad.: ... R_e

Perigee Dist.: ... R_e

Miss Dist.: ... R_e

V_∞: ... ^km⁄_s

Mission Values

Depart C3: ... (^km⁄_s)²

Arrival V_rel: ... ^km⁄_s

Phase Angle: ... °

* R_e = Earth Radii