Sounding Rockets

Since 1994 DTM develops on behalf of ESA scientific experiments for sounding rockets that are launched from Swediwsh Space Corporation's launch facility Esrange in the north of Sweden

CDIC2 and Source experiment

Prime Contractor SSC Swedish Space Corporation

On 15th of May 2008 the rocket MASER 11 has been launched from Esrange. The experiments onboard had full success. DTM was responsible for the design (including structural and thermal analysis), manufacturing and test test of the mechanical and hydraulic systems of two experiments: CDIC2 and Source.

CDIC2 (PI Dr. K. Eckert TUD Dresden - Germania) had the aim to study chemically driven interfacial processes that are present in many industrial chemical processes. Source had the aim to study convection and boiling phenomena in micrograviy condition. Among other goals this experiment will help understanding the behaviour of propellant in launcher tanks (PI Prof. M.Dreyer ZARM Brema, Prof. C.Colin IMFT Tolouse, Dr. P.Behruzi Astrium Brema).

Modulo CDIC2 completo presso DTM Technologies

Modulo Source durante t test nei laboratori SSC di Solna

CDIC and TRUE2 experiment

Prime Contractor SSC Swedish Space Corporation

On 2nd of May 2005 the sounding rocket MASER 10 was launched from Esrange. MASER 10 reached an apogee of 252 km and a top speed of approx. 2 km/sec. The experiments onboard spent six minutes in microgravity and worked perfectly during the flight. DTM was involved in the design, development and testing of the mechanical system of two experiments on-board this MASER rocket: CDIC and True 2. CDIC (Principal Investigator Dr. K.Eckert of Technical Univerisity Dresden - Germany) had the aim to study chemically driven interfacial convection processes. TRUE had the aim to study thermal radiation forces in unsteady conditions (Principal Investigators Prof. F.S.Gaeta, Dr.C.Albenese, Dr.F.Peluso of MARS Centre Naples, Italy).

CDIC experiment during testing at SSC Esrange laboratory

TRUE: Three of the six experiment cells mainly made in polymeric material.

Tem-Fer experiment

Prime Contractor Eads Space Transportation - Bremen

For the Prime Contractor EADS Space Transportation (former Daimler Benz Aerospace) an experiment was launched with full success in February 1998 and then in March 2003 (reflight). Professor Daniel Beysens of the CENG (Grenoble, France) is the Principal Investigator, that has specified the mechanical performance to be achieved by this module.

The two thermostats, whose temperature control has a maximum allowed variation of only 0.001 °C, are actuated by an acceleration system able to change both amplitude and frequency. The amplitude variation is achieved by a micrometric control of the crankshaft axial position, through a secondary motor and a special device. This three-dimensional shaft, grinded with a control accuracy in the order of the micron, couples - via connecting rods - the two slides supporting the thermostats.

Beysens module during vibration test
at Università di Modena

Dylco experiment

Prima Contractor SSC Swedish Space Corporation

The picture on the left depicts the Maxus 2 rocket being launched from Esrange, on the right is shown the Dylco Experiment which was mechanically developed by DTM. The Prime contractor for this activity was Swedish Space Corporation while the Principal activity investigator was Professor Langbain of ZARM University of Bremen (Germany).

Maxus 2 rocket launched from Esrange, Sweden

Dylco Experiment