Obviously taking oxygen in consideration. What prevents a small plane from being able to fly at a much higher altitude? I know some business jets can fly up to 40,000 ft. Does it have to do with the wings air foil? For example, can you fly a Cessna 172 at 20,000 ft or higher?
1$\begingroup$ Hi @Boeing787 - Engine is I imagine important - props don't have big compressors to make the air suitable ... But people have got close - see aviation.stackexchange.com/a/32719/56827 or aviation.stackexchange.com/a/61899/56827 $\endgroup$– Mr RJun 29, 2021 at 1:16
3$\begingroup$ Just about any Cessna can easily climb to 20,000’ if the engine is equipped with a turbo-charger. The Cessna T210 has a service ceiling of 27,000’. en.wikipedia.org/wiki/Cessna_210_Centurion $\endgroup$– Mike SowsunJun 29, 2021 at 1:20
1$\begingroup$ 40000 ft is perfectly normal even for airliners of all sizes. Business jets can go all the way to roughly 50k ft. $\endgroup$– TooTeaJun 30, 2021 at 8:13
3$\begingroup$ Of course the fact the cabin is not pressurised and people have a hard time being conscious at those altitudes without pressurisation is quite a factor. Adding pressurisation has quite a few consequences on the shape, weight and cost of the aircraft. $\endgroup$– jcaronJun 30, 2021 at 10:12
1$\begingroup$ Your answer implies that jets are large and other aircraft are small. This is not necessarrily the case. Think Hondajet en B-29 :) $\endgroup$– jwentingJul 1, 2021 at 12:41
We will take the case of an unsupercharged piston engine, as used in most small Cessnas and Pipers.
All engines need the oxygen in air to burn their fuel. As an airplane climbs, the air thins out and so there's less oxygen available, so the engine can burn less fuel and so it produces less power. There then comes an altitude at which there's not enough power available to pull the plane through the air any faster so as to make more lift in that thinned-out air and keep climbing. Roughly speaking, that is the plane's ceiling.
Now if we put a more powerful engine in the same plane, not only can it climb faster, but there's more power on tap at higher altitude even though its power output is still falling as it climbs. So it can keep pulling the plane through the air progressively faster as it climbs and thereby keep the wing producing enough lift to add altitude. In this way, a more powerful engine will lift the plane higher before running out of power and so exhibit a higher maximum ceiling.
Jet engines are enormously powerful and because of their compressor design, they can make the ambient air denser at high altitudes and so they can maintain their fuel burn rate and keep producing high power up to very high altitudes- far above the altitudes at which a piston-powered plane without a supercharger runs out of climb capacity.
You can add an air compressor (called a turbocharger or supercharger) to a piston engine's intake to trick it into thinking it is breathing sea level air when it is actually at 10,000 feet, and then it can keep climbing, as pointed out by Mike Sowsun- as long as the pilot has an oxygen tank on hand so he or she can stay alive up there.
This is a simplified picture, but not to worry- in a couple of hours, Peter Kaempf will be out of bed and will furnish a more complete reply!
6$\begingroup$ You can go higher if you add more supercharging stages. WWII fighters had service ceilings up into the 30s and some specialist aircraft with extended wings could get into the 40s. Problem is, for a civilian airplane you now need to pressurize it. Another limitation is cooling. The thin air becomes a struggle to get sufficient heat rejection from the cylinders and heat was a big enemy of the air cooled multi-stage supercharged engines above 30000 ft. It's not impossible but the various limitations make it impractical when jets do the job way better. $\endgroup$– John KJun 29, 2021 at 4:16
7$\begingroup$ @CGCampbell Thank you for pointing this out, but oddities like umlauts cannot be insisted on. I don't particularly mind the other spelling - it is used in my email addresses and credit cards due to the inflexibility of those. $\endgroup$ Jun 29, 2021 at 10:57
8$\begingroup$ Why should I add another answer when yours is already good enough? I would only link to lots of my older answers, like this or this one. I would, however, never say the plane needs to fly faster to produce enough lift for climbing. $\endgroup$ Jun 29, 2021 at 11:04
4$\begingroup$ Add to this that a plane shaped like a typical Cessna will be near its Mach limit at stall speed not much if any above FL400. This was the limitation on the U-2 -- the airframe was Mach limited, and absolute ceiling was where you couldn't stay above stall at that Mach number. $\endgroup$ Jun 29, 2021 at 11:09
You can add an air compressor (called a turbocharger or supercharger) to a piston engine's intake to trick it into thinking it is breathing sea level air- There's no trick here, by adding a compressor ahead of the intake you are actually feeding higher pressure air into the engine - no gags or tricks here, the plane thinks it is breathing denser air because it really is. $\endgroup$– J...Jun 29, 2021 at 18:24
What limits a small plane to be able to fly at a much higher altitude?
Power and lift on an aeroplane both decrease with increasing altitude, as shown in the image above, from my paper copy only old uni book of prof. Wittenberg. At 20,000 ft about 60% of take-off power is still available, at 40,000 ft about 35%.
Solution 1: install a turbo
From Torenbeek, Synthesis of Subsonic Airplane Design, fig. 4-10: maximum altitude of a Piper Navajo, piston engine with and without turbo. The vertical scale is a bit hard to read, it increases with 4,000 ft to a maximum of 24,000 feet. Which the more expensive turbo driven engine reaches, due to compressing the thin intake air at altitude.
Solution 2: install way more power, including multiple turbo's
Install enough power to begin with, and a propeller plane with piston engine can reach 40,000 ft as well, as shown by the data for the P-51 Mustang.
- Maximum speed: 440 mph (710 km/h, 383 kn)
- Cruise speed: 362 mph (583 km/h, 315 kn)
- Stall speed: 100 mph (160 km/h, 87 kn)
- Range: 1,650 mi (2,660 km, 1,434 nmi) with external tanks
- Service ceiling: 41,900 ft (12,800 m)
- Rate of climb: 3,200 ft/min (16 m/s)
- Lift-to-drag: 14.6
- Wing loading: 39 lb/sq ft (190 kg/m2)
- Power/mass: 0.18 hp/lb (300 W/kg)
- Recommended Mach limit 0.8
The service ceiling of 41,900 ft was courtesy of the Packard Merlin engine. Which is not being produced anymore, due to turbine type engines such as in the PC-12 being much lighter and less expensive for the same power rating.The PC-12 reaches 30,000 ft, is still too expensive for the average Joe Private Pilot though.
Conclusion: throw money at it, and it will fly higher...
22$\begingroup$ Not going to downvote a relatively interesting answer, however, I feel I must point out that this doesn't really answer the question. It's not what is the ceiling, it's what creates the ceiling. You start to intimate an answer with "due to compressing the thin intake air at altitude" but don't go into detail. $\endgroup$ Jun 29, 2021 at 9:25
1$\begingroup$ The Ta 152H had a service ceiling of 49k ft (with nitrous boost), if you want an even more extreme example $\endgroup$– llamaJun 29, 2021 at 16:29
1$\begingroup$ @CGCampbell "Power and lift on an aeroplane both decrease with increasing altitude" is the answer. $\endgroup$– KoyovisJul 1, 2021 at 10:13
$\begingroup$ If an airplane can take off, lift will not limit the altitude it can reach until the Mach effects of the coffin corner kick in. It is really just power that limits the altitude of small planes. $\endgroup$ Jul 4, 2021 at 4:24
The previous answers give an excellent overview of limiting factors regarding high altitude flight with powered civil aviation aircraft like a small Cessna.
Of interest might be that people have operationally used these aircraft at altitudes in excess of the aircraft's original-design flight envelope. One use in particular which comes to mind has been in special applications such as high-altitude aerial-photo surveys. A modified Cessna Turbo Stationair has been used in such high-altitude aerial surveys and was flown at altitudes above 37,000 ft (11.3 km). The plane's engine, modified to have a two-stage turbocharger, could maintain sufficient manifold pressure to fly at such altitudes.
The interior of the plane was essentially stripped of unused, excess-weight items (five of six seats) and other miscellaneous and unnecessary equipment. The camera bay, aerial camera and camera operating equipment, necessary flight instrumentation and radios, and sufficient oxygen (tanks), were items carried on such flights, along with required fuel. The owner of this plane commented that at such altitudes, the plane did not fly especially well, but it was manageable. He also commented on the interesting view looking down on commercial jet aircraft flying at altitude below.
Also of interest might be that other much lighter, essentially smaller, commercially built, single-place, unpowered aircraft have been routinely flown at altitudes well above 40,000 ft (12.2 km). These are sailplanes, and oxygen is required on such flights. Although generally less than 600 lb (270 kg) in weight (one-fourth the weight of a small Cessna), they have larger span wings (55 ft or about 17 m, more or less) with generally similar wing area compared to a small Cessna powered aircraft. Paul Bickle, retired director of the NASA Dryden Flight Research Facility, flew a Schweizer 1-23E sailplane to an altitude of 46,267 ft (14.102 km) on February 25, 1961. His flight was within a Sierra wave and was just over 2 hours from take-off to landing. Bickle's record for altitude gained, 42,303 ft (12.894 km), is unchallenged in a single-place glider. He suffered outside air temperatures of -65 deg C which frosted the inside of his canopy so badly he could not see the expansive view before him. He only had his instruments to guide his flight, and, because he could not close his cockpit outside-air vents, became so chilled and distracted by the cold that he had difficulty paying attention to piloting his sailplane. Of course, he was more attentive as his canopy cleared in warmer air at lower altitude. Also, Robert Harris flew a single-place Grob 102 sailplane to a record altitude of 49,009 ft (14.94 km) on February 17, 1986. His flight was also in a Sierra wave.
In 1952, Larry Edgar and Harold Klieforth set an altitude record in a two-place Pratt-Read G-1 glider, soaring to 44,255 ft (13.489 km) in a Sierra wave. However, on April 25, 1955, Larry Edgar's Pratt-Read glider was destroyed in the lee of the Sierra by a rotor-cloud at 17,000 ft (5.2 km) as he was investigating the rotor's turbulent structure at the base of a wave. The acceleration he experienced, in excess of -20g, ripped off his helmet, boots, gloves, and oxygen mask. As he drifted downward he could see parts of his glider being carried upward and worried if he pulled his parachute rip-cord, he might be carried upward as well. Fortunately, he was able to make a parachute landing and survived without breaking any bones. The extreme negative acceleration partially damaged his vision. Edgar was the only one in his sailplane when this happened.
As one can see, all caution must be used when flying an aircraft in conditions that are not within the original aerodynamic-design flight envelope of the aircraft. The plane will fly, but nevertheless, aerodynamic control is critical. This brings to mind the following caution that is especially true in high-altitude flight, and known all too well...
Aviation, although not inherently dangerous, is, to an even greater extent than the sea, terribly unforgiving of any carelessness, incapacity, or neglect.