The ultimate goal of Copenhagen Suborbitals is to launch a human on a suborbital ride to space. For this particular purpose we are designing the Spica rocket.
Designing a manned, suborbital space flight system is no easy task. Currently there are no manned suborbital space flight systems operational and actually only one system has ever been specifically designed and proven able to launch people into suborbital space flight, namely SpaceShipOne from Scaled Composites. The total list of manned suborbital flights is surprisingly short, it consist of just these eight flights:
- Mercury-Redstone 3 with Alan Shepard, May 5th 1961
- Mercury-Redstone 4 with Gus Grissom, July 21st 1961
- X-15 flight 90 with Joseph A. Walker, July 19th 1963
- X-15 flight 91 with Joseph A. Walker, August 22nd 1963
- Soyuz 18-1 with Vasili Lazarev and Oleg Makarov, April 5th 1975
- SpaceShipOne with Mike Melvill, June 21st 2004
- SpaceShipOne with Mike Melvill, September 29th 2004
- SpaceShipOne with Brian Bonnie, October 4th 2004
We’re flying an amateur astronaut into space on an home build, crowdfunded rocket. Want to see it happen ?
Become a Copenhagen Suborbitals Supporter
We need your help to build our Spica rocket. We all work for free in our spare time, but we still need to pay for materials. Become a supporter and be part of the most awesome space program in the world.
Spica is unique – the first third-sector manned spacecraft ever built. Our Spica launch program will make Denmark the fourth nation on Earth to send an astronaut into space on a domestic rocket, joining the ranks of Russia, China and the USA.
The first capsule we build will be a so called boilerplate model of the pressure hull made in steel. You can read more about it on the capsule page (click button below).
Inter tank section
The inter tank section will bridge the liquid oxygen and ethanol propellant tanks which will feed our DIY bi-liquid rocket engine. This is the first reel section of our big Spica rocket.
Spica will be powered by a 100 kN liquid bi-propellant engine running on liquid oxygen and ethanol just like our experimental BPM5 engine. Spica and the so far unnamed capsule will have a diameter of 955 mm, a total height of about 13 meter and a Gross Lift Off Weight (GLOW) of 4000 kg of which 2600 kg will be propellant. Thus Spica is a significantly larger rocket than our own HEAT-1X and will by a far margin be the largest rocket ever build by amateurs.
The engine will be fed in a pressure blow down combined with an active pressurisation system. Thus the propellant tank pressure will be maintained at the initial pressure for the first part of powered flight by a high pressure system. The implementation of such an active pressure regulation system results in a drastic overall performance increase and lower GLOW, it comes at a price of higher complexity though.
Attitude and control
Previously, for the Sapphire and Nexø rockets, we used a jet vane based attitude and control system. Since jet vanes incur an efficiency loss of typically 8-10% Spica will utilise a much more efficient gimbal system where the entire engine is tilted to provide thrust vectoring. Since this is a major design change compared to our previous rockets the gimbal system will be tested on a smaller rocket prior to the first flight of Spica. A technology demonstrator gimbal system was developed for our BPM5 rocket engine in 2016.
The current design is based on a very conservative engine efficiency of only 80%. This way we have a design which is very robust towards overweight or other performance issues. On the other hand, if we can prove the engine to have a higher efficiency than 80% we can chose to shave weight and propellants off the entire system and end up with a system that is lighter than anticipated.
Launch and landing
Spica will be launched from an upgraded Sputnik platform capable of supporting the weight and space required. With a Gross Lift-Off Weight (GLOW) of 4000 kg and a thrust of 100 kN Spica will climb out with an initial Thrust To Weight Ratio (TTWR) of 2.55. At T+20 seconds it will go super sonic and at T+90 seconds the engine will shut off at a velocity of about 3600 km/h and an altitude of 50 km. From here Spica will coast to apogee at 105 km at T+190 seconds. A few seconds later the ballute will be deployed in order to stabilize the capsule through the thin part of the atmosphere. Approximately 9 minutes after launch at an altitude of 4 km the parachutes will unfold and provide a gentle landing in the Baltic Ocean where the recovery team will be ready to secure the capsule and the astronaut.
At this point we still have a long and very exciting road ahead of us to reach this goal. As the only amateur based manned space flight program in the World we encourage you to join our effort and become a Copenhagen Suborbitals Supporter. Your support is our rocket fuel and is greatly appreciated!