Fascinating stuff!!
24 flights so far.

Go to the citation for the video, pictures and graphs:

https://mars.nasa.gov/technology/helicopter/status/373/balancing-risks-in-the-seitah-region-flight-24/

STATUS UPDATES | April 05, 2022
Balancing Risks in the 'Séítah' Region - Flight 24
Written by Ben Morrell, Ingenuity Operations Engineer at NASA's Jet
Propulsion Laboratory
This annotated overhead image from the HiRISE camera aboard NASA’s Mars
Reconnaissance Orbiter (MRO) depicts three options for the agency’s Mars
Ingenuity Helicopter to take on flights out of the “Séítah” region, as
well as the location of the entry, descent, and landing (EDL) hardware.
Mars Helicopter Route Options out of ‘Séítah': This annotated overhead
image from the HiRISE camera aboard NASA’s Mars Reconnaissance Orbiter
(MRO) depicts three options for the agency’s Mars Ingenuity Helicopter
to take on flights out of the “Séítah” region, as well as the location
of the entry, descent, and landing (EDL) hardware. Credits:
NASA/JPL-Caltech/University of Arizona/USGS. Download image ›
Ingenuity continued its journey towards the river delta this weekend
with Flight 24. This flight took place Sunday, April 3, and the data
arrived back later that evening. The flight was the fourth of five
sorties Ingenuity will make to cross the “Séítah” region of Jezero
Crater and arrive in the vicinity of its delta. This multiflight
shortcut across Séítah is being done to keep ahead of the Perseverance
rover – which is currently making great time on a more circuitous route
to the same area.

The Ingenuity and Mars 2020 teams have big plans for the helicopter at
the delta. But they have to get there first, and prior to Flight 24 a
crucial decision had to be made on which of three different flight plans
offered the best chance of a successful delta arrival.

The three options on the table were:

Option A: a single, long flight.
Option B: two shorter flights.
Option C: a very short Flight 24 to make the long flight out of Séítah
slightly easier than option A.
In deciding which of these options to greenlight, the Mars Helicopter
team had to consider multiple factors: thermal, atmospheric conditions,
flight time, drift, landing sites, and keeping up with the rover. We'll
explore each of these factors and what role they played in the overall
risk assessment and selection of our decision.

Thermal Limitations

For spacecraft, “thermal” refers to the management of the temperatures
of each component. Every part of Ingenuity has what is called Allowable
Flight Temperatures (AFT), which give a range of temperatures at which
each part is safe to operate. Even your phone or computer has a
recommended temperature range: Too cold or too hot and it will not work
as intended. Keeping “within AFTs” is critical for ensuring the health
of Ingenuity, which means we are very careful to manage this – for
example, by using heaters overnight when it is cold, and limiting
activities during the day, when it is warmer. A particular challenge for
Ingenuity is managing the temperature of its actuators, the servos and
motors that allow it to fly (see some of these here). These components
generate a lot of heat during flight, to the extent that the maximum
flight time is often limited by the maximum AFT of these actuators.

Atmospheric Seasonal Conditions

If you have been following this blog, you will know that we have been
operating with reduced air density since September, requiring an
increase in rotor rpm from 2,537 to 2,700. Flight 14, for example, was a
checkout flight to confirm Ingenuity could fly in these conditions. For
all flights since then, Ingenuity has been successfully operating with
2,700 rpm. Unfortunately, though, using a higher rpm causes the
actuators to heat more rapidly and reach their AFTs sooner, limiting
maximum flight time. Practically, this has limited us to flights of 130
seconds or less. Thankfully, we are toward the end of the Martian
summer, with its low air density, and starting to move into the Martian
fall, with higher air densities (see below), meaning we can now return
to the 2,537 rpm of our first 13 flights. This change in rpm allows an
increase in flight time to approximately 150 seconds. However,
atmospheric density isn't the only factor at play: The main driver of
the changes in density is the temperature of the atmosphere, which also
has a major impact on – you guessed it – the temperature of Ingenuity.

It is warmer now coming out of the summer than with our earlier flights
in the spring. So even though we have been flying at 10:00 a.m. local
mean solar time (LMST)- on Mars throughout the summer, Ingenuity has
been hotter than flights at 12:00 LMST in the spring. A warmer
atmosphere means warmer components, meaning we reach maximum AFTs
sooner. This means, flying at 10:00 LMST, we still can't fly for as long
as we did previously, such as during Flights 9, 10, and 12.

Models for the seasonal variation in atmospheric density on Mars between
summer (low density) and winter (higher density) predict that air
density will be high enough in late March for NASA's Mars Ingenuity
Helicopter to return to its original RPM.
Mars Atmosphere Density Model: Models for the seasonal variation in
atmospheric density on Mars between summer (low density) and winter
(higher density) predict that air density will be high enough in late
March for NASA's Mars Ingenuity Helicopter to return to its original
RPM. Credits: NASA/JPL-Caltech. Download image ›
Flight Time and Distance

With the current atmospheric conditions at Jezero Crater, the AFTs of
the actuators are the limiting factor for the total flight time. Let's
take a more detailed look at the different options for Flight 24 and beyond:

Option A: The long flight out of the delta requires 170 seconds of
flight, the maximum of our previous flights. This is not possible until
the atmosphere cools down further.
Option B: The two shorter flights are operating the same as our previous
“summer” flights: 130 seconds of flight time. This flight time is
possible without any changes.
Option C: The first flight, a short hop, is designed to reduce the
flight time needed for the second flight to 160 seconds. This is
possible if we: i) reduce the rpm to 2,537, and ii) fly earlier in the
sol to have lower atmospheric temperatures.
The team determined that by flying 30 minutes earlier, at 09:30 LMST,
the flight time could be increased by 10 seconds. However, Ingenuity had
never flown at 09:30 LMST before, so this would be a new “first.” And
flying earlier brings with it associated risks with the charge state of
the helicopter's batteries: Ingenuity uses power to heat itself
overnight and recharges its batteries with its solar panel, meaning the
batteries have less charge in the morning. If we choose to fly at 9:30,
we would first have to test it out – waking Ingenuity at this time
without flying, to check that it would have sufficient charge for a flight.

In summary, the different maximum flight time options available are:

130 seconds (baseline)
150 seconds (decreased rpm)
160 seconds (decreased rpm and earlier flight time)
Flight time is normally equivalent to distance traveled, but it also
depends on the maneuvers being performed. For example, rotating in place
(called “yawing”), is done (at least at Mars) slowly, taking a handful
of seconds with no distance traveled. For that reason, Mars Helicopter
flights with more yaw maneuvers don't travel as far in the same flight time.

All these factors come into play with option C – the short hop. This
flight would enable the longer 160 second flight, for several reasons:
1) it is a check-out test for flying back at 2,537 rpm, 2) it is a test
for flying at 09:30 LMST, and 3) it reduces the flight time for the
subsequent flight by doing the time-consuming yaw maneuvers and moving
slightly closer to the target for the second flight. All three of these
steps are required to enable a 160-second flight out of the Séítah.

Drift

As discussed in previous blog posts, Ingenuity was a tech demo expecting
to fly over flat ground. When flying over “non-flat” terrain such as
hills, cliffs, large boulders and large dunes, Ingenuity's estimate of
its position and heading can drift. This drift leads to a wider area
where it may land, called the landing ellipse. The farther it flies, the
larger the potential drift, and the larger the landing ellipse. The
Séítah region has many of these non-flat features (see the dunes and
rocks in the image at the top, or on the interactive map), making it
riskier for Ingenuity to fly over this region. An additional challenge
with the upcoming flights is the presence of hardware from
Perseverance's entry, descent, and landing (EDL), including the sky
crane, parachutes and backshell. The green dots (in figure 1) show the
predicted locations of this hardware from orbital imagery. Some of these
components are under the flight path of option B, which presents a
potential for unexpected performance from Ingenuity's laser altimeter (a
laser that measures the helicopter's height above the surface) and
visual odometry system, which could cause more drift.