An object to be parachuted comprising a parachute and a which parachute deploying apparatus, said parachute deploying apparatus comprising: a) a manifold with which is releasably coupled a single vessel within which pressurized gas is generated; b) a gas generator which cooperates with said vessel; c) a plurality of hollow tubes which extend obliquely and upwardly from, and are in communication with, said manifold, wherein said hollow tubes are oriented at a same angle with respect to a vertical plane to ensure uniform opening of said parachute; and d) a plurality of projectiles, each of which formed with a rod that is receivable in a corresponding hollow tube of said plurality of hollow tubes and to each of which is connected a cord that is also connected to a corresponding portion of said parachute, wherein the pressurized gas which is generated upon triggering of said gas generator is flowable through each of said hollow tubes to propel said plurality of projectiles in different directions and to cause said parachute to become deployed, wherein said object to be parachuted is an unmanned aerial vehicle, UAV,, said UAV comprising a plurality of rotors, each of which configured with rotating blades, and a safety apparatus being retained within a chamber attached to a support element of said UAV, wherein said safety apparatus comprises: i. said parachute in a folded condition; ii. said parachute deploying apparatus; and iii. a wireless communication unit for remotely controlling operation of said safety apparatus, wherein said safety apparatus further comprises: iv. a rotor deactivation unit synchronized with said parachute deploying apparatus, wherein deactivation of each of said rotors by said rotor deactivation unit ensures that said parachute which is being expanded following a gas generator triggering event will not become entangled with the rotating blades and become damaged. a) a manifold with which is releasably coupled a single vessel within which pressurized gas is generated; b) a gas generator which cooperates with said vessel; c) a plurality of hollow tubes which extend obliquely and upwardly from, and are in communication with, said manifold, wherein said hollow tubes are oriented at a same angle with respect to a vertical plane to ensure uniform opening of said parachute; and d) a plurality of projectiles, each of which formed with a rod that is receivable in a corresponding hollow tube of said plurality of hollow tubes and to each of which is connected a cord that is also connected to a corresponding portion of said parachute, wherein the pressurized gas which is generated upon triggering of said gas generator is flowable through each of said hollow tubes to propel said plurality of projectiles in different directions and to cause said parachute to become deployed, wherein said object to be parachuted is an unmanned aerial vehicle, UAV,, said UAV comprising a plurality of rotors, each of which configured with rotating blades, and a safety apparatus being retained within a chamber attached to a support element of said UAV, wherein said safety apparatus comprises: i. said parachute in a folded condition; ii. said parachute deploying apparatus; and iii. a wireless communication unit for remotely controlling operation of said safety apparatus, wherein said safety apparatus further comprises: iv. a rotor deactivation unit synchronized with said parachute deploying apparatus, wherein deactivation of each of said rotors by said rotor deactivation unit ensures that said parachute which is being expanded following a gas generator triggering event will not become entangled with the rotating blades and become damaged. i. said parachute in a folded condition; ii. said parachute deploying apparatus; and iii. a wireless communication unit for remotely controlling operation of said safety apparatus, wherein said safety apparatus further comprises: iv. a rotor deactivation unit synchronized with said parachute deploying apparatus, wherein deactivation of each of said rotors by said rotor deactivation unit ensures that said parachute which is being expanded following a gas generator triggering event will not become entangled with the rotating blades and become damaged.