1、 - - - -. . - . L. _. - 2.- . = - . MIL-P-25062B . - - 25 SEPTEMBER 1964 ?-+r.;*-*7.y*,+- li .-_ 2,;-.* .- - - - .- ., - .- _. 3.6.2.1 Depbyment bugs. Suitably designed deploymint bags shall be used to pack the parachutes used for the vidous stages of recovery and may include the first-stage par- a
2、chute when feasible. The bags -,shall cause ,S.;4, -,-y-,. . . . r. -_-A 7 bIIGP-25062B assemblies, or complete recovery systems shall be in accordance with the requirements of the specification of the missile, drone, or recoverable body on which it is to be used. - . . _. . . 6. NOTES - 6.1 Intende
3、d use. The recovery systems - - - -1 - covered by this specification are intended for use in safely decelerating a body and lower- ing it to land on the ground or water, applicable, in a relatively undamaged con- dition. as .- I 6.2 Definitions. . .- 6.2.1 Recovery sysh. A recovery system is the ass
4、embly of components and parts re- quired to return a missile or drone to the surface of the earth. This includes any shock- absorbing devices used to reduce the effect of landing impact, flotation equipment to keep - the body afloat, and a device to prevent drag- ging of the body by surface wind aft
5、er ground contact. 6.2.2 Deployment. Deployment is the por- tion of parachute operation beginning with extraction of the parachute from the com- partment in which it is stowed and ending the instant the suspension lines are fully stretched but prior to the inflation of the canopy. . . - P- . - - -.
6、i - :-I .- _ - 6.2.3 Drone. A drone is a radio-controlled aircraft used as a target. - _- 6.2.4 Recoverable body. A recoverable body - - is the missile, drone, or portions thereof being recovered. - 6.2.5 Minhum of dunzage. Damage con- strued to be a minimum of damage will not include any fiilure or
7、 damage to the primam = . f i structure of the airframe of the missile or :. . - drone and should be confined to items or structure that may be replaced or repaired . easily in the field. f P f 6.2.6 Reefing. Reefing is a temporary restric- . f tion of the drag area (parachute canopy) i t f -. . -_
8、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. .- MI.LP-25062B I and thus a reduction of the deceleration forces. Reefing is accomplished by reefmg Zisers may be formed by bundling a group of individual suspension lines or by using one or more pli
9、es of stronger material to which the suspension lines are attached. There may be one or more risers on any single parachute, multi-legged tributes the parachute forces equally to the several attachment points of a recoverable rings and a *=fing Illie. -. I-_-. _- e ._ - - _- A _- ._ - 62*7 Dbeeg* is
10、 the of the reefing line from the reefing rings (usually by cutting) to allow full inflation of . 6.2.8 Risers. Risers are flexible load-carry- ing members that transmit the drag force of the parachute to the recoverable body. body. - . . - - 64.9 Bale. A bridle is , ?- arrangement of flexible mater
11、ial that dis- - _- - ir the parachute canopy. c - .- .- a I -. .- _ _ -. _ _ ._ . - - - . -_ - ._.- ., _ - - - - -_ . P=p=hz activitg: . _ _ I _ - . Air Force-11 .- Cnstodians: hY-1cII Navy-Weps .r Project No. 1670-0101 ., r. - e Air Force-11 a- - _ Other intemate: - _ - - - Reviewera : -. - Army-m
12、 Navy-Weps Air Forcsll, 67 - . -. .I - -, =. ._ - _ - - - _. - -_ - - - - *._ - - . _-.- - - _- - . - - - - t- = . -_ _ r, -. - - ._ _- - _ t _-_*_ _ _._._ - ,_ . -_- I. -_ -.-_ -.-.- _ - - _ - _ _ . - - . .- _-. - -. - -. _- - - _ - I -_ _.+ - - - _ .- . - ._. - - - - , -; - _._ - - - -. _- - -I-
13、 _- - - - _ . _- .- . - - - - . - - - . - _- ._ - * - ._ - - .- - - - _ . _ _- - _- f 9 i 12 F-= -3 _. - -_ r - - .- - _. I_ _ . z ,._._* .,-.+- - -. -,-.- - -A- - . . - -. - _ _ -. _- - - - _. - . -5 $ . -_ ._ . .- .- _- *- I _ . - 3 - - *U. S. QOVERNMM PRINTINO OmCL: 751-p09164-T.04) I - - b“ * . ,. -_ 1 i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
