Ground test of a deployment parachute system of the Cluster micro SRM rocket at 20.06.11
Ground test of the deployment parachute system of the experimental rocket Solaris_2S_3000 with SRM. The rocket structure dead mass is 9 kg. Mass of the ejected rocket´s segment is 3.5 kg.
Ground test of optical apogee detector HEAD (Hawk EYE Apogee Detector) Made in Bulgaria installed on the microhybrid rocket DAGA_2.
Parachute ejection ground test for the Solaris_H_1SM HRM experimental rocket.
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