The highly complex and extremely powerful P5.2 upper stage test stand is the latest test stand at DLR in Lampoldshausen and completes the portfolio of the DLR test site with its ability to qualify entire upper stages. The test stand was developed and built as part of the development of the future European launcher Ariane 6 on behalf of the European Space Agency ESA.
With the successful test on September 1, 2023 at DLR in Lampoldshausen, the newly designed upper stage of Ariane 6 has taken an important step towards qualification and first launch. With two ignitions of the Vinci engine and two ignitions of the APU, a highly complex requirement profile was mapped on the P5.2 test stand.
Video: Hot run test of the Ariane 6 upper stage at DLR in Lampoldshausen
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Video: Hot run test of the Ariane 6 upper stage at DLR in Lampoldshausen
With the successful test on September 1, 2023 at DLR in Lampoldshausen, the newly designed upper stage of Ariane 6 has taken an important step towards qualification and first launch. With two ignitions of the Vinci engine and two ignitions of the APU, a highly complex requirement profile was mapped on the P5.2 test stand.
Credit:
ESA/ArianeGroup/DLR - Hill Media 2023
Areas of application
Low-pressure test bench for testing entire upper stages under ground conditions with the engine running
Fueling and defueling tests of cryogenic upper stages
Fuels
Liquid hydrogen
maximum 2.7 kilograms per second
Liquid oxygen
maximum 10.3 kilograms per second
Number of test positions
one test position
Current test object
The P5.2 test stand was specially designed and built by DLR to test the Upper Liquide Propulsion Module (ULPM) of the Ariane 6 upper stage. The upper stage consists of the Vinci engine, which can be ignited several times, the tanks for liquid hydrogen and liquid oxygen, pipes, valves and the electronic and hydraulic monitoring and control systems.
Facts & Figures
Building
Surface area
5.000 Quadratmeter
Length
35 meters
Width
45 meters
Height
30 meters
Test cell
Width
14 meters
Depth
14 meters
Height
24 meters
Maximum thrust
250 kilonewtons
Firing axis
Vertical
Supply
Helium (expandable)
8 cubic meters
Nitrogen (expandable)
40 cubic meters
Liquid oxygen (from P5)
180 cubic meters
Liquid hydrogen (from P5)
600 cubic meters
Measurement signal acquisition
about 1,000
Financing
The test stand is financed from the German ESA contributions to the Ariane 6 development program. The DLR Space Agency is responsible for providing and coordinating these funds on behalf of the German government.