Rigid Thermal Airships
Founded in 2025, based in the UK, our mission is to design and build large rigid airships
Replacing helium with hot air as the lifting gas
Rigid Thermal Airships are Rigid Airships (also called zeppelins) that use hot air as the lifting gas
In this case the air is heated to between 200-300C above ambient
- Because of their buoyancy airships are capable of vertical takeoff and landing, this allows them access to places without transport infrastructure such as roads, rails and airports and allows them to hover in place. This also allows them to fly "point to point" without the need to use several transport modes
- They are capable of carrying large and heavy cargo over long distances at competitive levelised cost
- Their bouyancy means that a propulsion failure does not result in loss of lift, a safety advantage
- Their slower speed and use of propellers instead of jet engines makes them quieter than planes
Here is a table comparing attributes of several lifting gases
Hydrogen | Helium | Steam | Hot air | |
---|---|---|---|---|
Lift/volume (kg/m3) | 1.1 | 1.0 | +200C: 0.78 +300C: 0.86 |
+200C: 0.51 +300C: 0.63 |
Initial minimum cost per cubic metre ($0.20/kwh) | $0.60¹ | $10 | +200C: $0.07 (1.24MJ) +300C: $0.06 (1.11MJ) |
+200C: $0.008 (0.14MJ) +300C: $0.01 (0.18MJ) |
Initial minimum cost per Kg of lift ($0.20/kwh) | $0.55¹ | $10 | +200C: $0.09 +300C: $0.07 |
+200C: $0.02 +300C: $0.02 |
Not flammable | x | ✓ | ✓ | ✓ |
Inherent lifting gas | ✓ | ✓ | x | x |
No Envelope pressurisation | x | x | x | ✓ |
Renewable inexhaustible supply | ✓ | x | ✓ | ✓ |
Available anywhere | ✓² | x | ✓² | ✓ |
Ease of envelope access | Hard | Hard | Medium | Simple |
Density variation | Low | Low | Medium | High |
(All at sea level and 20C ambient)
¹ Electrolysis, ² With water
Why Hot Air
Hot air is chosen as the lifting gas for several reasons
1. It is not flammable, this is important and is the biggest problem with hydrogen
2. It is available everywhere, all the time, by far the easiest lifting gas to obtain, no filling required
3. It is by far the initially cheapest lifting gas per volume and per unit of lift
4. It's lift can be varied by adjusting its temperature and does not have the big barrier of phase change energy that steam has
5. It takes much less heat energy to warm up than steam, so heats/cools faster, cheaper and much higher % heat recovery is possible
6. It does not require pressurisation. When ascend, air pressure drops and some internal air exits to equalise the pressure. This means the lift/volume is percentage of external air density instead of fixed value when pressurised. This means as ascend, lift/volume decreases more slowly than other lifting gases and proportional lift/volume to them is increased
The envelope shape is the same prolate spheroid shape common on most airships
However the length/width ratio is reduced compared to helium airships
This decreases the surface area/volume ratio, decreasing required volume for same lift and decreasing surface area for heat loss
This increases drag on the ship which requires more powerful engines. However required thrust power scales with speed³ so a small decrease in speed reduces required thrust power significantly
The envelope is made of rigid metal beams running around and across it
Metals are used for the beams which maintain their strength at high temperatures
Around the surface, thin metal panels are placed to enclose the envelope
Below the panels, insulation is placed to significantly reduce heat loss
The envelope has a hole in the bottom to allow internal air pressure to equalise with the outside
To ascend the airship the air inside is heated, decreasing its density and increasing its bouyancy
To descend, do the opposite
Vectored propellers are placed around the airship for thrust and control
To increase and maintain heat of the envelope air a fuel must be burnt
Hydrogen is used as the fuel for heat and to provide electricity for the propellers
If the airship is in regular use, it is expected that the internal temperature is maintained just below where neutral buoyancy is achieved, this makes taking off again faster
Solar heat collection can be used to cover majority of the heat maintenance requirements during daytime
One or more heat recovery methods are used when heating or cooling internal air
The payload of the airship is placed under the envelope, any cargo and passengers go here
Our airship will use hydrogen as its fuel
This allows for 3 major advantages over fossil fuels
Firstly, hydrogen has the highest energy density of any fuel, this minimises weight of the fuel and therefore maximises range and payload capacity
Secondly, hydrogen produces zero CO2 emissions when either burned or run through fuel cells, it can also be produced with little to no CO2 emissions
Thirdly, hydrogen can be produced by the customer themselves, if the customer purchases their own zero fuel cost electricity sources such as wind and solar, and hydrogen production technology using this electricity, then they are able to produce their own fuel at zero cost
We aim to meet at least these specifications
Note that costs are conservative upper estimates and that all is subject to change
Attribute | Value |
---|---|
Envelope Volume | > 2,000,000 m³ |
Payload | > 100 tons |
Purchase Cost | - Airship: TBD - Fuel self production requirements: TBD |
Heat cost (+200C) | Without own fuel production - Initial (no heat recovery) < $40k - Ongoing < $2k/hour With own fuel production* - Initial: $0 - Ongoing: $0/hour |
Max internal temperature | > 350C |
Altitude Ceiling (MSL) | 10,000 ft |
Air Speed | Cruise > 50 knots Max > 60 knots |
Max thrust | > 50,000 hp |
Endurance (cruise) | > 16 hours |
Fuel | Hydrogen (Liquid or Gas TBD) |
Average levelised running cost | Without own fuel production < $3/ton/mile With own fuel production* $0/ton/mile |
Ongoing heat energy from solar (daytime) | > 50% |
Heat recovery | > 50 % |
* Excluding ongoing maintenance costs of hydrogen production facilities
Designing and Building any new aircraft is often a multi year process due to various complexities including engineering, regulatory and financial
Our goal is to deploy the first production airship no later than 2035
The airships will be designed and built in the UK, a country with a long history of aviation and airship innovation
We are currently looking for seed funding
This will allow us to...
- Obtain an office
- Continue design of the airship
- Begin discussions with potential buyers, suppliers and regulators
- Hire initial required staff
Further funding would allow us to...
- Obtain/Construct a hangar
- Build a smaller prototype
- Get customer preorders
- Build a full scale prototype
- Complete testing and obtain certification from regulators
- Build the first production airship
- Become profitable and provide a return on investment
If you want to invest in the future of airships please contact us