Structure of INDELA SP-35 system at UAV landing mass of 35kg ensures the following performance characteristics | ||
Maximum speed of parachute activation | m/s | 60 |
Minimum speed of parachute activation | m/s | 15 |
Minimum height of parachute activation above landing field level | m | 100 |
Maximum (barometric) height of parachute system activation | m | 3500 |
Barometric height of landing field location above the sea level | m | up to 2000 |
UAV load, while activation of parachute system | kgf | not more than 400 |
Amplitude of system’s snap-back angle at the moment of landing | degree | not more than 30 |
Functionality at the temperature | °С | -40 - +60 |
Operation of the parachute system.
After separation of a parachute container cap from UAV, auxiliary parachute enters the flow, which, after being filled, sequentially stretches the cover with the main parachute from the container, shrouds – from the cell chamber, then – cupola from the cover.
Structure and operation of parachute system elements. Main parachute structurally represents “duplex cross” with a vent. Eight paddle parachute cupola is made of F-111 fosta nylon fabric produced in RSA with low level of air permeability ad is strengthened by the frame from LTKP-10-70 belt (with the strength of 70 kgf). Shrouds (16 items) are produced from hi-modulus polyethylene (Dyneema) with the strength not less than 120 kgf. Cover designed for main parachute packing represents a conic container with the length of about 2m. In the upper part, the cover has a loop for connection with VP and in the lower part – two eyelets for coupling of the cover. Honeycomb for placement of main parachute’s shrouds are abut at the side face of the cover. Honeycombs are covered by the skirt.
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