Great news from Virgin Galactic on Sunday. Although according to the widely used definition, their spacecraft didn’t quite get into space. Most international authorities define that space begins at an altitude of 100 km (the Karman line), whereas VSS Unity reached an altitude of 86 km, but a fantastic achievement nevertheless !!. For those who may have missed it the following article on the BBC website https://www.bbc.co.uk/news/science-environment-57797297 gives a good summary of the flight.
Well done to all involved!!!
The definition of where space begins is an interesting subject. So, I’ve decided to reblog a revised version of a a blog post from 2019 on this topic
Possible definitions of space
The Earth’s atmosphere consists of gas and there is obviously no fixed boundary where it ends, and space begins. As we get higher in altitude its density falls until it eventually reaches the very low density of five particles per cubic centimetre found in interplanetary space. In the diagram below, I’ve illustrated some different altitudes and I’ll discuss whether each of them could be considered to be in space.
8.8 km – The summit of Mount Everest. At this altitude the air pressure is only one third of that at sea level. A young fit person acclimatised to high altitude could not survive for more than 30 minutes without needing extra oxygen.
10.6 km – Boeing 747 cruising altitude. The air pressure at this altitude is around 24% of that at sea level and a human would be dead within minutes from lack of oxygen. Even so, this altitude is not generally considered to high enough to be defined as in space.
20.7 km – Concorde maximum altitude. This was the maximum altitude which the supersonic aeroplane Concorde achieved and it occurred during a test flight in 1973. At this altitude air is so thin that the sky is dark blue in daytime and the air pressure is only 7.6% that of sea level.
Concorde was in service between 1976 and 2003 and could travel at a speed of 2,180 km/h – more than twice the speed of sound. It had a maximum cruising altitude of 18.3 km and was advertised as travelling ‘on the edge of space’.
At 20.7 km the boiling point of water is only 30 degrees Celsius, so a human being whose body temperature is normally 37 degrees would be subject to an extremely unpleasant fate unless they were enclosed in a space suit or a pressurized cabin – the water in their eyes, mouth, throat and the lining of the lungs would literally boil away. Therefore, it could be argued that Concorde on this test flight was travelling in space.
41.4 km – world balloon altitude record. This was achieved by Alan Eustace, a Senior Vice President of Google, in 2014. At this altitude the air pressure is only 0.237% of the sea level and the air density is so low that the sky appears black in the daytime. Although this altitude is not generally considered to be high enough to be in space, Eustace felt that at he had reached space. On his return, he said
‘..It was beautiful. You could see the darkness of space and you could see the layers of atmosphere, which I had never seen before.’
as quoted in the New York Times
100 km – an altitude known as the Karman line which is usually taken as the boundary of space. I will discuss this later.
150 km – approximate minimum altitude for a satellite to complete an orbit. At this altitude the Earth’s atmosphere has about one billionth of its density at sea level.
When a satellite is in a low orbit around the Earth, its rapid movement through the very tenuous traces of the Earth’s atmosphere results in friction, which causes the satellite to lose energy and spiral back to Earth. The higher a satellite’s orbit, the thinner the atmosphere, which means that there is less friction and it remains in orbit longer. At 150 km, the thickness of the atmosphere is such that a typical satellite would theoretically be able to complete a single orbit but it would be spiralling down towards the Earth quite rapidly. At altitudes below 150 km, a typical satellite would not be able to complete a single orbit. In fact this minimal orbital altitude is only approximate, as the amount of friction slowing down a satellite also depends on the size and shape of the object. At an altitude of 150 km, a heavy streamlined satellite could stay up for longer than one orbit.
400 km – International Space Station (ISS). At this altitude the atmospheric density is a miniscule half a trillionth (0.000 000 000 000 5) of its density at sea level, but this very tenuous gas still causes a small amount of atmospheric drag on the ISS. The ISS loses altitude at the rate of around 2 km per month and needs to fire its own rocket motors (or those on visiting spacecraft) a few times a year to raise its altitude. If it didn’t do this, the ISS would continue to lose altitude and would return to Earth in a few years, breaking up in the process.
1000 km – at this altitude the atmospheric density is so low that a satellite will remain in orbit for over 1000 years without returning to Earth.
Air density and pressure at different altitudes
Data from http://www.braeunig.us/space/atmos.htm
Altitudes above 100 km are significantly affected by solar activity. The figures in the table above have been taken for low solar activity.
The Karman Line
The Fédération Aéronautique Internationale (FAI), the international body setting standards and keeping records in the field of aeronautics and astronautics, defines space as starting 100 km above the surface of the Earth. At this altitude the atmospheric density and pressure are more than a million times lower than they are at sea level. This altitude is called the Karman Line after the Theodore von Kármán (1881-1963), a Hungarian-American mathematician, aerospace engineer, and physicist. He calculated that at approximately this altitude it would not be possible for an aeroplane to fly because the air density is too low for enough lift to be generated by airflow over the aircraft wings (see the notes below for more details).
Even so, this 100 km boundary is somewhat arbitrary and isn’t accepted by everyone. Interestingly, the United States Federal Aviation Authority (FAA) defines space as starting not at the Karman line but at 80 km above the Earth’s surface. Virgin Galactic therefore felt confident enough to state on their website on 13 December 2018 that a test flight that day had reached space, having achieved 82.7 km, and that their pilots were therefore astronauts:
The historic achievement has been recognised by the Federal Aviation Administration (FAA) who announced today that early next year they will present pilots Mark “Forger” Stucky and Frederick “CJ” Sturckow with FAA Commercial Astronaut Wings at a ceremony in Washington DC.
However, when it starts commercial operations Virgin Galactic will take space tourists to a maximum altitude of 110 km, 10 km above the Karman Line. This will avoid any argument about whether they have travelled high enough to reach space. As described in a previous post the flight will have a price tag of $250,000, which is a little too expensive for me.
Richard Branson the founder of Virgin Galactic who has publicly stated that he will be a passenger on the first commercial spaceflight of VSS Unity. My wife feels that he seriously needs to change his hairdresser 🙂
The motion of an aircraft through the air is governed by four forces.
- Thrust is the forward force provided by the engines which pushes the aircraft forward.
- Drag is the force caused by air resistance as the aircraft moves through the air. It slows the aircraft down.
- Weight is the downward force due to gravity.
- Lift is the upward force caused by the fact that when an aircraft moves through the air, the air pressure is higher on the underside of the aircraft’s wing compared to the topside. This higher air pressure on the underside pushes (or lifts) the aircraft upwards.
The lift (L) generated by airflow over the wings of an aircraft is given by the lift equation
L = ½ ρv2ACL
Where the terms are as follows.
- p is the atmospheric density
- v is the aircraft’s velocity with respect to the surrounding air
- A is the surface area of the aircraft’s wings
- CL is a number known as the lift coefficient, which depends on the size and shape of the wings and properties of the surrounding atmosphere.
For an aircraft to remain at a constant altitude the amount of lift generated must be equal to the weight of the aircraft.
From the lift equation, as the density of the atmosphere falls, an aircraft must move faster to generate the same amount of lift. At an altitude of around 100 km the atmospheric density is so low that an aircraft’s velocity needs to be greater than 28,200 km/h to provide enough lift. This is the velocity needed to get into orbit, so an aircraft moving at altitude of 100 km would actually be in orbit around the Earth and its passengers and crew would be weightless.