PROJECT
ATLAS
The first high-power research rocket in Romania
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LIFTOFF
MAIN ENGINE START
Atlas.
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PURPOSE
To transform a simple launch into a real data-driven experience.
MISSION
To bring real-world science into the hands of students.
IMPORTANCE
Because learning changes when the data is real.
Nose Cone
Length: 280mmMass: 85gCd: 0.42
DART-1
Payload Deep Atmosphere Research Telemetry. ESP32-S3 dual-core processor. 100Hz sampling across all channels. LoRa 868MHz downlink. SD card backup.ESP32-S3100Hz sample rateDual storage
Recovery System
Dual-deploy Parachute Drogue at apogee, main at 250m AGL. Jolly Logic Chute Release — no pyrotechnic charges required.Drogue: 60cmMain: 120cmDescent: 5 m/s
Propulsion
Cesaroni Pro38 I285-CL. Reloadable composite motor. 512 Newton-seconds total impulse in a 1.8-second burn.
Thrust: 285N avgImpulse: 512 N·sBurn: 1.8s
Aerodynamics
G10 fiberglass 3 trapezoidal CNC-cut fins at 120° spacing. Static stability margin exceeds 1.5 calibers for safe transonic flight.Material: G10Count: 3 × 120°Margin: 1.5 cal