Here is a thread-based version of my talk at #orbitaldebris2019 yesterday. I haven't been able to include everything, but I hope it gives you a sense of what I talked about (Image Credit: 'Gravity' Warner Bros. Pictures 2013) #spacedebris
Only 10% of future traffic in LEO goes to altitudes >1000 km. In absolute terms, that is only 17 objects per year added to the population above 1000 km. With respect to the existing population, the peak spatial density (at 800 km) is 4 times higher than anywhere else (data: ESA)
Repeating the 2010-2017 launch traffic cycle with 90% PMD compliance & no explosions leads to what appears to be a fairly 'stable' population. The total no. objects increases at only 5 objects per year. Collision fragments are deposited at ever-slower rates. All looks good!
The projection of the debris population is not a future prediction. 'Blade Runner' was (arguably) about what it means to be human; the future setting allows that theme to be explored. The principle is the same for the simulation (Image Credit: 'Blade Runner, Warner Bros. 1982)
The simulations allow us to understand the fundamental behaviour of the 'system'. A bath is a great example of a simple system. The water level is what we are interested in, and it is controlled by water inflow (via a tap) and outflow (via a drain).
The water level rises if the tap is 'on' and the drain is 'closed'. The water level falls if the tap is 'off' and the drain is 'open'. The water level (can) remain constant if the water inflow is equal to the water outflow, i.e. dynamic equilibrium.
Human population dynamics are similar to space debris population dynamics. If the birth rate is higher than the death rate, we have exponential growth in the population. If the death rate is higher than the birth rate, we have exponential decay.
If the birth rate is the same as the death rate then we have dynamic equilibrium – the population (size) stays the same. These are the fundamental responses of the human population system and they are the same for space debris population system
Previously it looked like the space debris population system was near to 'dynamic equilibrium' but this is what happens if we just allow the simulation to continue - exponential growth. This means that collisions must be adding debris faster than it is removed by the atmosphere
Collisions occur throughout LEO (in the simulation) but the debris accumulates at an increasing rate only above 1000 km - the region that receives hardly any new launch traffic and did not have a high spatial density to begin with
The level of collision activity is still substantial at altitudes < 1000 km (75% of all the collisions occur here)
We can see that the interval between collisions decreases for altitudes > 1000 km. At the start of the simulation, collisions occur once every 50 years. By the end of the simulation it is once every 5 or 6 years.
The 'Kessler Syndrome' scenario happens in the simulation at a much slower rate than was portrayed in the movie 'Gravity', but the interval between collisions will continue to decrease if the simulation continues and perhaps it is not difficult to imagine such pace after all
A large proportion of the collisions in the simulation involved spacecraft and upper stages that had already manoeuvred to comply with the '25-year rule' (these are the points circled in the graph). As a 'countermeasure', the 25-year rule doesn't appear to be working
So, we do have a problem and it will take some effort to find and implement a solution (Image Credit: 'Apollo 13', Universal Pictures 1995)
But, "The future has not been written. There is no fate but what we make for ourselves." This is a call to everyone who can help us tackle the #spacedebris problem (Image Credit: 'Terminator 2: Judgment Day', TriStar Pictures 1991)
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Welcome to this month's look at #Starlink conjunction risk mitigation manoeuvres. Through 30 April 2023, I estimate that Starlink satellites have made a total of > 45,000 manoeuvres to mitigate the risk of colliding with other space objects [1/n]
A better relationship to consider is the one between the (cumulative) number of manoeuvres and the (cumulative) number of Starlink satellites launched. The growth is a non-linear function of the number of Starlink satellites [2/n]
Here, I looked at the manoeuvre estimates/reports in 6-monthly intervals, corresponding to the reporting periods used by SpaceX. Additionally, I added a prediction to the end of 2024 based on an exponential fit through 30 April 2023. [3/n]
I've been thinking about the new proposed @FCC "five-year rule" for #SpaceDebris mitigation & wanted to share some analysis & thoughts. Whilst I think the intentions are good I believe the implications of the change are poorly understood. Let me explain... [1/n]
As @brianweeden's excellent thread explains, "The new proposed ruling would require all FCC licensed satellites that end their life in LEO to re-enter the atmosphere within 5 years, and ideally ASAP." [2/n]
Latest analysis for #Starlink & #OneWeb shows these two constellations accounted for 42% of all close approaches within 5 km predicted by #SOCRATES at the end of August, with Starlink alone accounting for 29%. [1/n]
On average, #SOCRATES predicts that each #Starlink satellite will now experience 1 close approach within 5 km with a non-Starlink object every day, and each #OneWeb satellite will experience 3.4 close approaches with a non-OneWeb object every day. These rates are increasing [2/n]
Here's the same data from [2/n] plotted with respect to the number of satellites in each constellation in orbit, clearly showing #SOCRATES predicts that #OneWeb satellites experience more close approaches (within 5 km) per satellite than the #Starlink satellites [3/n]
A follow-on from yesterday's thread with a note about averages. In a #SOCRATES report from 30 June 2022 the average collision probability for each #Starlink conjunction was 3.7E-6 but the range of values can be broad (chart shows data since 2019) [1/n]
#SOCRATES predicted some events with a collision probability > 1E-2 (1-in-100) & some with a probability < 1E-7 (1-in-10,000,000). The average value might seem to be almost negligible & you might think all conjunctions would be similar, but that's not the case [2/n]
In addition, some #Starlink & #OneWeb satellites experience more conjunctions than others. Most satellites experience relatively few encounters but a few satellites are involved in a relatively large number (charts shows data for 7 days from 30 June 2022) [3/n]
Welcome to my (delayed) monthly analysis of @CelesTrak#SOCRATES conjunctions. Since 1 March 2019, SOCRATES has predicted about 9 million unique conjunctions within 5 km involving active or derelict payloads. This is a thread focused on those involving #OneWeb & #Starlink [1/n]
#OneWeb payloads have accounted for ~500,000 unique conjunction predictions since 1 March 2019 (5.5% of all predictions made), while #Starlink payloads have accounted for ~1.1 million (12.5%) [2/n]
On 1 March 2019 #SOCRATES predicted ~3860 unique conjunctions within 5 km. On 30 June 2022 the corresponding number was ~10,160, an increase of ~160%. #Starlink accounted for ~2570 (25%) & #OneWeb accounted for ~1250 (12%) [3/n]
In advance of my monthly analysis of #Starlink conjunction data I wanted to share some additional analysis undertaken over the last few days. It's a work in progress but here's a thread looking a little deeper at the #SpaceX approach to #Starlink orbital space safety [1/n]
My focus has mostly been on understanding the implications relating to the choice of the probability threshold for collision avoidance manoeuvres. With the #SOCRATES#Starlink data now running across nearly 3 years we can gain some insights that may be useful [3/n]