DLR rocket flight in ATHEAt program demonstrates CMC nose, movable body flaps

Source | DLR (CC BY-NC-ND 3.0)

On Oct. 6, the German Aerospace Center (DLR, Braunschweig) launched a 13.5-meter-long research rocket for the Advanced Technologies for High Energetic Atmospheric Flight of Launcher Stages (ATHEAt) program from the Andøya launch site in northern Norway.

The experiment flew for ≈4 minutes, including 2 minutes of high-speed flight with the peak speed exceeding Mach 9, exposing the vehicle to gas temperatures exceeding 2000°C and extreme aerothermal loads on its structures and materials — similar to those encountered by spacecraft re-entering Earth’s atmosphere. During the flight, the research rocket reached a maximum altitude of more than 30 kilometers.
 

The shimmering gray nose cone of the rocket was made largely from a fiber- reinforced ceramic matrix composite (CMC) manufactured entirely at DLR using specially developed in-house processes.

This high-performance material not only withstands very high temperatures but is also strong and relatively lightweight. The scientific payload onboard the ATHEAt flight included two cooling experiments which researchers used to investigate how the extreme high temperatures at the nose of the rocket can be managed through active cooling.

The ATHEAt flight experiment’s front body also included four movable flaps made of DLR’s CMC which were successfully deployed during the flight and experienced very high temperatures. In the future, such flaps could be used to make space transportation vehicles more controllable.

The CMC nose cone and deployable body flaps on the ATHEAt first rocket. Source | DLR (CC BY-NC-ND 3.0). For more details, see ATHEAt flight experiment.

To achieve the highest possible temperatures, the research rocket flew along a specially planned, shallower trajectory, enabling it to fly at high Mach numbers for an extended period at relatively low altitudes. A newly developed DLR sensor network provided essential data to determine the precise moment of ignition for the second stage. This “sensor cube” uses a defined starting position and measures the acceleration and rotation rates in flight to calculate the position of the rocket in space. At the end of its flight, it splashed down safely in a designated and secure area of the Norwegian Sea.

Successful first flight

“With the ATHEAt flight experiment, we have succeeded in flying at high Mach numbers for much longer than in our previous projects,” says Ali Gülhan, ATHEAt project manager and head of the Supersonic and Hypersonic Technologies Department at the DLR Institute of Aerodynamics and Flow Technology. “We have now reached a new milestone and collected data for further R&D.”

This data harvest was made possible by the more than 300 sensors installed by the DLR team into the flight experiment. Also on board were miniaturized, noncontact sensors such as infrared cameras, laser scanners and radiation thermometers. A modular data acquisition system developed by DLR recorded the measurements and transmitted the processed data by radio to ground stations below.

“The conditions simulated in the ATHEAt flight experiment are comparable to those that thermal protection systems on future reusable space transport systems will have to reliably withstand during reentry into Earth’s atmosphere,” explains Gülhan. The reentry phase, with its extreme aerodynamic and aerothermodynamic conditions, is also a crucial point of development for the space industry. “With projects like ATHEAt, we are specifically working on closing this global technology gap.”

DLR combines flight experiments like ATHEAt and its predecessor projects, supported and continuously refined with sophisticated simulations, design processes and component testing on the ground.

CMC rocket nozzle DLR exhibited at JEC World 2024. Source | CW

DLR exhibited a CMC rocket nozzle for the ATHEAt program at JEC World 2024. It was designed and produced for a hybrid engine using carbon fiber and a matrix of carbon and silicon carbide (C/C-SiC) aiming to increase nozzle efficiency by drastically reducing abrasion and component weight for reusability.