MNV-0909 · CZ-4C R/B

OG-5 Halcyon — in-track burn, executed

All maneuvers

Delta-v0.28m/s

Propellant0.044kg

Axisin-track

Executed14h 11m ago

Statusexecuted

Burn performed. Post-burn state vector confirmed by tracking.

Effect on the event

Pc before2.9×10⁻⁴

Pc after6.1×10⁻⁸

Conjunction: CJ-4442 (cleared)
Spacecraft: OG-5 Halcyon
Secondary: CZ-4C R/B
Operator: R. Okafor

Propellant cost

This burn0.044kg

Remaining9.88kg

SK runway7.0yr

9.880 kg after burnreserve 2.2 · capacity 12.4 kg

Already drawn down — the remaining figure above is post-burn.

Orbit response

Gauss variational · Clohessy–Wiltshire

Δ semi-major axis528.8m

Δ period0.664s

Δ eccentricity7.5e-5

Drift per orbit4.983km

Along-track at TCA (0.0h lead)0.00km

An in-track burn separates by changing the orbital period, so displacement grows as Δx = 3·Δv·t. Lead time, not delta-v, is what buys miss distance — the same burn an hour later is worth proportionally less.

Propulsion

Tsiolkovsky

Specific impulse220s

Thrust2.400N

Vehicle mass337.5kg

Propellant0.0438kg

Burn duration39s

Mass fraction1.3e-4

System: Hydrazine monopropellant, 4x0.6N
Δv capability remaining: 49.7 m/s
Avoidance burns of this size left: 175

Burn is short relative to the orbital period, so the impulsive approximation used above holds.

Downstream conjunctions

not modelled

No downstream screening on file for this burn. Historical burns retain their record but not the re-screening that followed.