MNV-0908 · IRIDIUM 33 DEB
OG-1 Meridian-1 — radial burn, declined
Delta-v0.11m/s
Propellant0.016kg
Axisradial
Executed1d 14h ago
Statusdeclined
Reviewed and rejected — the estimate did not justify the propellant.
Effect on the event
Pc before4.4×10−5
Pc after9.2×10−8
- Conjunction
- CJ-4438 (cleared)
- Spacecraft
- OG-1 Meridian-1
- Secondary
- IRIDIUM 33 DEB
- Operator
- M. Reyes
Propellant cost
This burn0.016kg
Remaining6.14kg
SK runway2.1yr
6.140 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 axis0m
Δ period0.000s
Δ eccentricity1.4e-5
A radial burn changes eccentricity without changing the period to first order, so it produces no secular along-track drift.
Propulsion
Tsiolkovsky
Specific impulse220s
Thrust2.400N
Vehicle mass313.7kg
Propellant0.0160kg
Burn duration14s
Mass fraction5.1e-5
- System
- Hydrazine monopropellant, 4x0.6N
- Δv capability remaining
- 27.3 m/s
- Avoidance burns of this size left
- 246
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.