with reference to the drawings wherein like numerals represent like parts throughout the several figures , an aerial delivery system in accordance with the present disclosure is generally designated by the numeral 10 . with reference to fig7 a and 7b , the aerial delivery system or cartridge 10 comprises a cartridge base platform 12 , a ramp platform 14 and a restraint subsystem 16 . the aerial delivery system 10 is intended for use with aerial delivery cargo containers 18 of the type shown in u . s . pat . no . 8 , 480 , 035 , although it may be used with other aerial delivery containers , aerial delivery systems and air cargo systems as explained below . the cartridge base platform 12 includes an aerial delivery platform 20 having conventional interface elements ( not shown ), allowing the platform 20 to interact with the aircraft &# 39 ; s cargo handling system 22 . in the example shown in fig3 , the cartridge base platform 12 has a 32 ft aerial delivery platform 20 . with additional reference to fig4 , the cartridge base platform 12 also includes a conveyor 24 having a series of roller tracks 26 and side guidance features 28 on the top surface 30 . the roller conveyors 26 are removable , and can be configured for different payloads . attachment provisions 32 for restraint straps are also included , fig5 and 6 . the embodiment shown in fig3 - 8 includes two central roller tracks 26 and rotating bollards 34 forming two rows of side guidance features 28 spaced to support a single column of 48 ″ wide containers 18 centered on the platform 20 . another embodiment includes four rows spaced to support two columns of 48 ″ wide containers symmetrically loaded on the platform . side guidance features 28 includes vertical bollards 34 with an integral rolling element 36 which contacts the base board 38 of the container 18 . side guidance bollards 34 can also be reconfigured for one or two columns of 48 ″ wide payloads . another embodiment of the side guidance feature 28 includes rails extending the length of the platform which have a low friction surface in place of any moving mechanical elements . the low friction surface could comprise nylon or uhmw polyethylene , for example . the ramp platform 14 , fig7 a , 7 b and 8 , also includes an aerial delivery platform 20 ′ with conventional elements for interfacing with the aircraft cargo handling system 22 . the ramp platform 14 is sized to fit on the aircraft cargo ramp 40 . the top of the ramp platform 14 is also fitted with roller tracks 26 ′ and side guidance features 28 ′ to match the cartridge base platform 12 . restraint features are not necessary . the restraint subsystem 16 , fig3 , and 5 - 10 , includes a series of webbing straps 42 with clevises , tensioning devices , and release mechanisms 44 which attach the containers 18 to the cartridge base platform 12 during handling and flight , yet can be rapidly released to allow airdrop . straps must provide upward , aft and lateral restraint to meet standard air transportability requirements . forward restraint is provided by a forward bulkhead 46 . this can be either a standard buffer stop assembly typically used in container delivery system ( cds ) airdrops which is separately installed , or an alternate bulkhead structure incorporated in the base cartridge platform 12 the restraint subsystem 16 may include wireless gate releases ( wgrs ) to allow release of straps via remote command . another embodiment makes use of conventional cds airdrop techniques , using guillotine knifes attached to the static line retrieval winch . straps may need separate provisions such as elastic bungee cords to move the released straps out of the way of moving payloads to prevent fouls . typically in operation , fire suppressant containers 18 are loaded onto the cartridge 10 , for example the eight caylym guardian ™ fire suppressant containers shown in fig3 , and attached thereto by the restraint subsystem 16 ( see fig5 ). the system 10 requires dunnage between adjacent containers 18 , in order to successfully transmit forward aircraft acceleration forces to the forward restraint 46 . the rigged cartridge 10 is then loaded onto the aircraft 48 using conventional ground handling equipment , fig6 . the cartridge 10 has sufficient mechanical strength for a rigged cartridge 10 to be lifted by overhead crane onto a k loader or similar ground handling equipment . if the aircraft &# 39 ; s cargo handling system 22 includes a buffer stop assembly ( bsa ) rather than an integral forward barrier , a temporary forward restraint must be applied in order to rig the cartridge 10 . the cartridge 10 is then locked into the aircraft cargo handling system ( chs ) 22 . it is probable that the dunnage between the cartridge 10 and the restraint 46 will require adjustment in order to ensure a good load path ; otherwise no further rigging activity is required . this is where significant time saving is achieved . conventional gravity extraction systems require extensive rigging , and inspection , in the aircraft . in order to provide roller continuity across the ramp 40 , the system 10 also requires a ramp platform 14 to be loaded and locked to the cargo handling system 22 on the aircraft ramp 40 , fig7 a and 7b . after the aircraft ramp 40 is raised , fig8 , the aircraft is ready for departure . upon arrival at the drop zone ( fig9 a ), the ramp 40 is lowered ( fig9 b ) and the vertical and lateral restraints of the restraint subsystem 16 are removed / retracted ( fig9 c ), placing the system 10 in a pre - drop condition ( fig1 a ). when the order is given to drop the containers 18 , any remaining components of the restraint subsystem 16 removed / retracted and the containers 18 are conveyed out of the aircraft 48 ( fig1 b ). after completion of the drop , the aircraft ramp 40 is raised and the aircraft 48 returns to the base ( fig1 ). conventional container delivery system airdrop requires restraint straps be applied after the cargo is loaded into the aircraft . this is followed by an extensive inspection . both these operations are time consuming and must be completed before the aircraft can depart on the next sortie . the subject system 10 allows the rigging and inspection to be conducted ahead of time before the aircraft arrives , reducing the amount of time the aircraft spends on the ground between missions . it will be appreciated that various of the above - disclosed and other features and functions , or alternatives thereof , may be desirably combined into many other different systems or applications . any bulk cargo airdrop where rapid turn around is required could be addressed . for example , distributing enzyme to control ‘ red tide ’, deploying survival equipment or shark repellant dye to aid search and rescue efforts in a maritime disaster , or distributing herbicide on illegal crops could be addressed . also that various presently unforeseen or unanticipated alternatives , modifications , variations or improvements therein may be subsequently made by those skilled in the art which are also intended to be encompassed by the following claims .