UNCLASSIFIED
AD NUMBER
LIMITATION CHANGESTO:
FROM:
AUTHORITY
THIS PAGE IS UNCLASSIFIED
AD429215
Approved for public release; distribution isunlimited.
Distribution: Further dissemination only asdirected by Naval Ordnance Test Station, ChineLake, CA, DEC 1963, or higher DoD authority.
NOTS per DTIC form 55
UNCLASSIFIED
A D 429215
DEFENSE DOCUMENTATION CENTER FOR
SCIENTIFIC AND TECHNICAL INFORMATION
CAMERON STATION. ALEXANDRIA. VIIGINIA
UNCLASSIFIED
NOTICE: Üben govemnent or other drawings, epecl- flcatlons or other data are used for any purpose other than In connection with a definitely related government procurement operation, the U. S. Government thereby incurs no responsibility, nor any obligation whatsoever; and the fact that the Govern- ment may have fonaulated, furnished, or in any way supplied the said drawings, specifications, or other data is not to be regarded by implication or other- vise as in any manner licensing the holder or any other person or corporation, or conveying any rights or pemlsslon to manufacture, use or sell any patented invention that may in any way be related thereto.
L¥-tf
NAVWEPS REPORT 8439 NOTS TP 3395
COPY 57
AIRCRAFT QUALIFICATION INFORMATION PACKAGE
GLADEYE WEAPON SYSTEM
(Bomb Dispenser Mk 4 Mod 0 and
Bomb Dispenser Canister Mk 2 Mod 0)
by
Dennis E. Glendenning -»_^__ Weapon.s Development Department
y JAN 3 Ü 1964
TISIA B
ABSTRACT. A summary of the information necessary for an aircraft manufacturer or other qualified agency to establish compatibility and performance characteristics of an aircraft loaded with a Gladeye Dispenser System is presented. This report should be used as a basis for any such study.
ItoleaSBd to A-TTA for further AlMMin 0ul llBitationa beyond U»M l«P« '■■■ regulavi oii^. ___^„
U.S. NAVAL ORDNANCE TEST STATION
China Lake, California December 1963
U. S. NAVAL ORDNANCE TEST STATION
AN ACTIVITY OF THE BUREAU OF NAVAL WEAPONS
C. BLENMAN, JR., CAPT., USN WM. B. MCLEAN, PH.D. Commandmr Technical Director
FOREWORD
The Gladeye Weapon System was designed and developed by the Naval Ordnance Test Station to provide the Navy with a modular-type dispenser of stockpiled ordnance for use on present high-performance aircraft.
This report summarizes the information required by an aircral' manufacturer (or other agencies) to establish the compatibility of the Gladeye Weapon System with the bomb racks and the aircraft that are to carry this weapon.
The Gladeye development program has been carried out under Bureau of Naval Weapons WepTask RM3773-009/216-1/F008-2i-002 as a part of the over-all Free-Fall RDT&E Program established in I960 to improve the effectiveness and efficiency of the air-attack conventional weapon capability of the Naval Carrier Task Forces.
This report has been reviewed for technical accuracy by Dr M M Rogers and R. C. V. Reed.
Released by F. H. KNEMEYER, Head. Weapons Development Dept. 6 December 1963
Under authority of WM. B. McLEAN
Technical Director
NOTS Technical Publication 3395 NAVWEPS Report 8439
Published by Weapons Development Dep^nmem Manuscript 40/MS 63-50 Collation Cover, 13 leaves, abstradt cards First printing 120 numbeTe<i copies
Security classification UNCLASSIFIED
o CE
O <
H
m <
■a •i
i o Ul
H
u
ÖÖ
> rt
CD
H o
^3
00
d > S <
u
h a
5 5 •« ^ rt o rt ^
^ n ^ 0 C O «* ^4
p
zA\ * o 3 ?, c
S E » o
£ 2 ^ ••:' s u ■ S <• h « r
■ " o a m
in
a, o u
-o
O
a) XI
■Nl < ' n) O
H u c ^ u i; c "i
W
Q H
01 •«
4) 3 C a"
>-. 11 aj in in 3
5-3 o a j-,
>^ m V
^s 8
rti L.
Ü
IT!
u nl
a C
0
c «2 O n)
•5 i IT)
H
u ■ C u
■d
0 nJ
M u n)
C o
W 0
H o a;
u
d a c ■a >-. o n) >
ir.
H O
J3
ij53
B. ^ ■
rt en oo
1 X
6 ft . ro X)
>N O
4)3
3 aS
»2? a x u a, I:
Hx U
S
c C 2 3 en a, ««H
u 0
in 0)
a o u
XI u a) u
o5 > nJ td t-
10 K
h 0) in
a D
a| in
Q XI I o
n E OJ •"* in >• n c o aj n) ■
0) >- 11
o 2:
>.z
nJ ro
00
« W
6^
1 X
1,8.1
0 rt^ O StH
•3 a *_. IQ
S * C N
-a .
0) vO
0
u u ai;
o 2 0 c
S*-j pS tn
■a
x tn Hx
u
■
S 0
a, tn
<-a
W 85?
H U <
H
rt.« tu en
•H 0 <u 4-* 4-« . u
y >H d
il n)
tn tn >, n)
u a Oi u to d c s 11
u 11
in .^ 5 ■s S
1» 3 o d ow
a-" 52 p/3 >« m
■^ t: ,2 Q o &
D et U
a)
U
c o
o 2 0 c
o3 E » o u nl
5 "• K
d fo
02
fi S * -s 3 (j m tn 01 t, tu r
ni O
O
„ XI
W u .
E ro OJ ro
• n) >- m H ^ ü ^ u ^ c «1 ^ O u r; <"" ooT,
tn in
>s nl
*>* u <u <u in tn d
s^ •0-3 ^x ?» tn ■
o
{I
a H
en
o 2:
^
nl ro
00
a w
11 55
X
IT!
> nl 2
in
in
c o a i
1)
li U u 1) in d u D- tn
Q x> g o
CQ
x) c nJ
C ^
s * 01
X) .
Ü
1 X
►«8.»
0 «'S O W^H
«Xl f!) ^ -^ lH si« ^SE^ d o c S u ^ Sx •«
m o
-a .2 3 £ «i pa tn Hx
u
-O ui 1)
c c tn 1) Vn
1 nl ;xi
0) n) «rl • ^ «3
as
H u <
ro ■<
a,
^ -M *J U tn tn h D-r1
n) O <u +-• *J
c . o n) >>n)
y ^ o S ^
ta >N nJ
ro D
S^H
X) ^ (U D tn 01 3
8.J1 to ^3
0 9 >N tn ■
XJ t* i Jj
'd 0
■ nl b
tn
u
a, o u
XI h m u
o u
-a h m u
NAVWEPS REPORT 8439
INTRODUCTION
The development of the Gladeye Weapon System has been carried out at the Naval Ordnance Test Station to meet the requirements of the Navy for a low-cost, all-purpose dispenser of stockpiled ordnance for use with present tactical aircraft. The weapon has the capability of dispensing a variety of Army- and Navy-developed bomblet systems and devices in large loads per aircraft station.
To establish compatibility and performance characteristics of the Gladeye weapon system with an aircraft, the following areas must be investigated by an aircraft manufacturer (or other agencies) as desig- nated by the Bureau of Naval Weapons:
1. Spatial and mechanical clearances I. Static strength 3. Stability and control 4. Dynamic loadings 5. Electrical loads 6. Performance effects
The purpose of this report is to furnish the data that are required by the cognizant agency to carry out these compatibility studies. The general description, operation, physical characteristics, and other requirements of the weapon system are presented. The sequence of operations for loading and preparation are also provided to aid in compatibility studies.
GENERAL DESCRIPTION
The Gladeye (Fig. 1 ) is a modular-type dispenser system consisting of two major units: (1) seven identical cylindrical sections (Canisters Mk 2 Mod 0) plus an aerodynamic nose and tail fairing, and (2) the dispenser assembly (Bomb Dispenser Mk 4 Mod 0) to which the canisters are attached and which incorporates the rack adapter. The dispenser assembly contains seven canister ejector assemblies. Each ejection assembly is actuated by two Bomb Ejection Cartridges Mk Z Mod 1 wired in parallel to provide a sympathetic - redundant ignition system. The canister retaining hooks are released by a gas-operated sear. The canister ejector assemblies are fired in sequence (rear to front) by an intervalometer located in the forward fairing of the dispenser. The intervalometer provides four modes of ejection: single (pilot option), slow salvo (300 ms), medium salvo (100 ms), and fast salvo (50 ms).
,• NAVWEPS REPORT 8439
Q <" er 0) £ o i^J >. :ti c^ "•li § n; O < 2 CD o a
n) <u ^ V >. ■ •o »1
a
NAVWEPS REPORT 8439
The Gladeye Dispenser Assembly is shipped with the ejectors and the intervalometer installed- Expendable component s --i. e . , bomb ejector cartridges, loaded canisters, nose and tail fairings-- are shipped as required.
The Bomb Dispenser Canister loaded gross weight can vary from 195 to 32 lb total weight depending on the payload used. The following canister weights will be used for compatibility analysis: 196, 150, 88. 5. 75, 50, and 32 lb.
The Gladeye weapon was designed to dispense a long narrow pattern of munitions from low altitudes, thus maiung it ideal for strafing and close air-support missions. These missions often require additional external fuel tanks. For this reason, any performance and stability analysis should include--in addition to a full weapon complement--a more optimum loading including external fuel tanks.
The Gladeye dispenser system is uesigned fur aircraft carriage at speeds up to Mach 1 with a delivery speed range from 100 to 600 knots IAS. Delivery altitudes range from 50 to 10, 000 ft AGL. Environ- mental conditions of release have included all of those specified in MIL-T-7743.
PRKPARATION AND LOADING OPERATIONS
PREPARATION OF DISPENSER
Both of the 1. Remove dispenser from crate. Insert two bon
suspend the dispenser at a convenient height above deck. öoth ol the lugs should be used to suspend the weapon as the CG will shift during loading. Back off sway brace bolts as far as possible.
2. Observe the intervalometer through the opening in the forward fairing and set the position indicator to SAFE.
3. Remove the seven safety pins from the ejector assemblies.
4. Open each of the ejector-latching assemblies by prying up on the visual sear indicator located on top of the dispenser, as shown in Fig. 1.
LOADING OF CANISTERS ON DISPENSER
1. Hoist the canister into position No. 4 of the dispenser, allowing canister lugs to rise into the guides cast into the bottom of the ejector- latching assembly. Observe that an upward pressure on the canister
NAVWEPS REPORT 8439
causes the hooks to close allowing the sear to drop into the locked position. This sear motion is observed from the top of the dispenser. When the sear is down and locked, the safety pin must be inserted.
WARNING: After this operation, safety pins must not be removed until immediately prior to takeoff.
Repeat the above procedure on stations No. 5, 3, 6, 2, 7, 1, in that order. Note that canisters No. land? must have fairing rivets facing outboard.
2. Open the cartridge access doors and remove the firing leads (spark-plug type). Unscrew the cartridge holders and remove the cylinders (bayonet-type fastening).
WARNING: Do not open cartridge access doors in a high-energy electromagnetic area.
3. Remove the protective caps from the two Mk 2 Mod 1 Bomb Ejection Cartridges and insert the cartridges facing each other into the cylinder. Replace the cylinder into the cartridge holder and replace the holder into the ejector-latching unit. Replace the firing lead. Repeat steps 2 and 3 for all ejector-latching units.
4. Lower the weapon onto skid and move to loading area.
5. Assemble the frangible fairings onto canisters No. 1 and 7 using fairing attachment rivets. Rotate the fairing until a click is heard or the arrows are aligned.
6. If the weapon is to be hoisted aboard the aircraft using Mk 8 bomb hoists, insert the special hoisting lugs into the recesses that are cast on either side of position No. 4. Sling the small cable attaching lugs together under the weapon. The Mk 8 hoists can then be used to hoist the weapon with no further rigging. These lugs are shipped as part of the maintenance kit.
WARNING: Weapon must be racked and sway braces tightened before firing plug is inserted.
NAVWEPS REPORT 8439
7. The intervalometer is adjusted through the opening in the forward fairing. Move the mode selector to the mode desired and the position indicator to the arm position.
DISASSEMBLY
In case a weapon is returned with a partial load or for any reason it must be disassembled, the following procedure will be used.
WARNING: Replace safety pins and set intervalometer to SAFE immediately upon return of aircraft. NOTE: The intervalom- eter is set SAFE by pushing in on the position selector and turning clockwise.
1. Remove weapon from aircraft and suspend above deck using both bomb lugs.
NOTE: To avoid damage be sure the inter- valometer is returned only after disengaging ratchet by pushing the selector in.
2. Remove cartridge holder from weapon and remove cartridges from cylinder. Replace both holder and cylinder after cleaning.
3. Remove fairing by releasing spring lock and rotate to disassemble.
4. Remove safety pins from weapon.
5. Provide support for each canister before prying up visual sear indicator to release manually.
6. Stow components until needed.
CLEARANCE
Scale drawings of the loaded Gladeye dispenser are included as Fig. 2 and 3. Note the clearance necessary for safety pin removal as well as sear motion during the ejection process. It will also be noted that an intervalometer mode and selector adjustment is necessary through the access port after the weapon is aboard the aircraft. This adjustment requires the use of a medium-size screwdriver, and that the operator look directly into the port to avoid a parallax error in the setting. It is imperative that the mode and selector adjustment be
I NAVWEPS REPORT 8439
WS0M St AH INOKirOR -y .330
r/A/, jr/}SSry
p/jv/r* y^s^e
V/£W Z?/*?
FIG. 2. Loaded Bomb Dispenser, End View.
completed after the weapon is hung on the rack and connected to its power source because of the RADHAZ danger. It should also be noted that the cartridges are installed prior to installation on aircraft for RADHAZ reasons.
WEIGHT, CG, AND MOMENT OF INERTIA
The configuration of the Gladeye Weapon System establishes a weight, CG, and moment of inertia which vary as canisters are ejected. For this reason the weapon weights, horizontal CG, and moments of inertia are presented in tabular form in Fig. 4 through 9 for 32-, 50-, 75-, 88. 5-, 150-, and 195-lb canister weights. The values presented in the tables of these figures represent test data and hence are limited to the accuracy of the instruments used. It is felt, however, that this represents a truer picture than an analytical approach.
The weapon CG shift for the vertical plane, however, was derived analytically because of the difficulty in accurate measurement in this plane and is presented in Fig. 10-16. It should be noted that the dis- tance from the weapon CG to intersection of lines of action of sway brace forces as required by MIL,-A-8591 is presented as values A through G.
MX-* *fOOO
*r* ■tsasr
k ■k:
J7V
XC. D D
^
i
n
MS» <,,*> /
/
>a
cew.
FIG. 3. Loaded Bomb Dispenser Mk 4 Mod 0 (G
NAVWEPS REPORT 8439
7 /VSao
3 D
:>
FIG. 3. Loaded Bomb Dispenser Mk 4 Mod 0 (Gladeye).
I—A
NAVWEPS REPORT 8439
32 LB. CANISTER
7 6 5 4 5 2 1 WT. CG ICG
X 215 5 1.12 4,260
X X 247 49.18 4,420
X X X 279 48.25 4,440 X X X X 311 49.43 4,550
X X X X X 343 51.00 4,8 30
X X X X X X 375 53.12 5,5 40 X X X X X X X 410 56,25 6,860
FIG. 4. Weapon Horizontal CG and Moment of Inertia Data, 32-lb Canisters.
NAVWEPS REPORT 8439
50 LB. CANISTER
7 6 5 4 3 2 1 WT. CG. ICG
X 230 48-94 4,6 00
X X 288 46.62 4,8 90 X X X 338 46.12 4.89 0
X X X X 388 47.50 5.060
X X X X X 438 49.62 5,6 30
X X X X X X 488 52.44 6,6 70
X X X X X X X 541 56.00 8.8 00
FIG. 5. Weapon Horizontal CG and Moment of Inertia Data, 50-lb Canisters.
NAVWEPS REPORT 8439
hT.frt (28.73) (35f 5] (50.55'
18.66
75 LB. CANISTER
7 6 5' »5 2 1 WT CG. Ic.G.
X 266 46.50 5,100
X X 341 43.81 5,450
X X X 416 44.19 5,540
X X X) ( 491 45.81 5,820
X X X) <x 566 48.69 6,770
X X X) <x X 641 52.88 8,670
X X X) (X X X 716 56.00 11,680
FIG. 6. Weapon Horizontal CG and Moment of Inertia Data, 7 5-lb Canisters.
10
NAVWEPS REPORT 8439
(vr.sr) (28.73) (39.65) ^0.55)
88.5 LB. CANISTER
7654321 WT. CG. ICG.
X 277 44.68 5,260
XX 365 42.38 5.570
XXlX ^54 42.94 5,620
XXXX 542 45.31 6,200
XXXXX 613 48.38 7,250
XXXXXX 719 51.94 9,430
XXXXXXX 810 56.00 13,050
FIG. 7. Weapon Horizontal CG and Moment of Inertia Data, 88. 5-lb Canisters.
11
NA VW EPS REPORT 8439
150 LB. CANISTER
7 6 5 4 3 2 1 WT. CG. ICG
X 337 41.25 6,040
X X 487 38.92 6.330
X X X 637 40.68 6,560
X X X X 787 43.87 7,610
X X X X X 937 47.2 5 9,800
X X X X X X 1087 51.50 13,800
X X X X X X X 1240 56.00 19,750
FIG. 8. Weapon Horizontal CG and Moment of Inertia Data, 1 50-Ib Canisters.
1Z
I NAVWEPS REPORT 8439
7 6 e> 4 3 2 1 WT CG. D
183 2,85 -4.14 X 215 4.15 -2.64
X X 247 5.10 - 1.69 X X X 279 5.8 4 - 95 X X X X 311 6.4 2 - .37 X X X X X 3 43 6.90 + .11 X X X X X X 375 7.30 .51 X X X X X X X 407 7.63 .84
FIG. 10. Weapon Vertical CG Data, Aero <iOA Rack With 32-lb Canisters.
14
NA VW EPS REPORT 8439
7 f. 5 4 3 2 1 WT. CG. E
183 2.85 -4.14
X 233 4 73 -2.06
X X 283 5.92 - .87
X X X 333 6.78 - .01
X X X X 383 7.39 + .60
X X X X X 433 7.90 Uli
X X X X X X 483 8 29 1.50
X X X X X X X 5 33 8.55 1.76
FIG Ae
j. 11. Weapon Vertical CG Data, ro 2^A Rack With 50-lb Canisters.
15
NAVWEPS REPORT 8439
120°
7 6 9 4 ? 2 1 WT. CG. F
183 2.85 -4.14
X 258 5.41 -1.38
X X 333 6.86 + .07
X X X 408 7.71 92 X X X X 483 8.28 1.4 9
X X X X X 558 8.75 196 X X X X X X 633 9.10 2.31
X X X X X x X 708 9.36 2.57
FIG. l<i. Weapon Vertical CG Data, Aero ZOA Rack With 75-lb Canisters.
16
NAVWEPS REPORT 8439
T 6 5 4 3 2 1 WT. CG. B
183 2.85 -4.14
X 273.5 5.66 -1.13
X X 362.0 7.10 + .31
X X X 450.5 7.97 1.18
X X X X 539.0 8.56 177
X X X X X 627.5 8.98 2.19 X X X X X X 716.0 9.29 2.50 X X X X X X X 804.5 9.54 2.75
FIG. 13. Weapon Vertical CG Data, Aero 20A Rack With 88. 5-lb Canisters.
17
NAVWEPS REPORT 8439
CG. CANISTER
7 6 5 4 3 2 1 WT. CG G
183 2.85 -4.14
X 333 6.76 - .03
X X 483 8.24 + 1.48
X X X 633 9.02 2.26
X X X X 783 9.50 2.74
X
X
X X X * 933 9.83 307
X X X X X 1083 10.05 3.29
X X X. x X X X 1283 10.20 3.44
FIG. 14. Weapon Vertical CG Data, Aero 20A Rack With 150-lb Canisters.
18
NAVWEPS REPORT 8439
CANISTER CG.
7 6 5 43 2 1 WT CG. C
IB5 2.85 - 4.14
X
380 7.31 + .52
X 575 8.74 1.95
X X X 770 9.45 2.66
X X X X 965 9.87 3.08
X X X x> < 1160 10.15 3.36 X X X X ) <x 1355 10.35 3.54 X X X X (X < 1550 10.50 3,71
FIG. 15. Weapon Vertical CG Data, Aero 20A Rack With 195-lb Canisters.
19
NAVWEPS REPORT 8439
20
7 6 5 4 3 2 1 WT CG. A
185 2 85 - 1.99 X 380 7.31 - .33 X X 575 8.74 + 1.10
X X X 770 9.45 1.81 X
X
X X X 965 9.87 2.23
/\ X X X 1160 10.15 2.51 X X X X X X 1355 10.35 2.71 X X X X X X X 1550 10.50 2.86
FIG. 16. Weapon Vertical CG Data, Aero 7A Rack With 195-lb Canisters.
I NAVWEPS REPORT 8439
All distances are in units of inches, CG locations are in terms of weapon stations, and moments of inertia are in slug-in2. Weights are in pounds.
SPECIAL REQUIREMENTS
EJECTION LOADS
As can be seen from the weapon configuration, when a Gladeye canister is ejected, the rack on which the weapon is mounted reacts to the ejection force as well as the couple so produced.
Figure 17 shows the Gladeye ejector and its method of function. The gas pressure produced by the Mk 2 ejection cartridges provides the release action as well as the ejection force. Since the sear piston overcomes its spring force at approximately 63% of peak pressure, and since the volume change during ejection is small as compared to the total volume, the ejection force of the ejector does not vary appreciably with different canister weights. These characteristics Iso have the effect of maintaining an almost linear ejection acceleration with respect to canister weight. This ejector is remarkably little affected by temper- ature variations. For these reasons the canister ejection force may be considered a constant as represented by a plot of typical pressure and ejection force versus time shown in Fig. 18.
Figure 19 shows a plot of loads experienced by the aircraft under a fast salvo ejection utilizing an Aero 7A Rack. The setup for this test is shown in Fig. 20.
ELECTRICAL REQUIREMENTS
The Gladeye dispenser wiring diagram and intervalometer sche- matic is presented in Fig. 21. Gladeye was designed to utililize the bomb-rocket firing circuit of Navy aircraft, and currently utilizes pin A of the rocket plug for a positive 28 VDC and pin E for ground. This was done to establish compatibility with a wiring change suggested by NOTS and with fleet-configured aircraft. It was found that, with the existing current-limiting resistor in the rocket-fire current, insufficient current was available for reliable cartridge ignition. However, with the resistor removed the power was adequate. Since this problem was common not only to Gladeye, but also to other items utilizing this cir- cuit to squibs, it was suggested that the unused pin D be fitted with a firing lead bypassing the current-limiting resistor. Action on this suggestion is still pending.
21
NAVWEPS REPORT 8439
SEAR
,MK2 MODI BOMB EJECTION CARTRIDGE (GASGENERATOR)
O-RING MS 2877S-I26
CARTRIDGE HOLDER ASSEMBLY
VISUAL SEAR INDICATOR
SEAR PISTON
FIRING PULSE CAUSES CARTRIDGE IGNITION. GAS PRESSURE BUILDS UP.
GAS PRESSURE MOVES PISTON AGAINST CANISTER, CAUSING COLLET TO GRASP LANYARD PIN OF MK 2 CANISTER. SEAR MOVES IN UPWARD DIRECTION DUE TO GAS PRESSURE ON SEAR PISTON. SEAR MOVEMENT LEAVES HOOKS FREE TO UNLATCH. CANISTER IS EJECTED AWAY BY PISTON, AND LANYARD UNRAVELS FROM CANISTER. LANYARD OPENS CANISTER.
FIG. 17. Canister Ejector Assembly.
22
NAVWEPS REPORT 8439
04B
FIG. 18. Typical Pressure and Ejection Force Versus Time (195-lb Canister, Ambient Temperature, 18.85-ft/sec Velocity).
<i3
NAVWEPS REPORT 8439
ii"
f w s
U U i 11 LILI n 1 it 11 IT 1
■f4444-| Ff ' REACTION OF FORWARD MOUNT 4 i I ~ I 1 1 1 i 1 C - OCA/^Tlrtfcl ^1- r
"*'. M . t M£ = MOMENT A BOLT MOUNTING CENTER I ■■ ^^v
T ,1 rS, ---f-- .„ J_ .. ._ ■ s. . x _. :
J kS. i::t__ _:__ ' - JS* I * ^ N. fi"::" \^r ^ ^r
a " < \. P
■"^ ̂ Hi ! ( -t c - :::::::::::::::::: :::^ -- (F( ,<!- in •^ SNJ * ' * * 1^ aci /
U J 1 11 .zu. ** - II it H. \; /
' t \ ^ 4 0 s ::z_!S::::xit:i r xt** ~
^ >» t > K • "V / ^J: JT 1 ", T«, ^T -^Tk^'Jl S ::::: \^ ^^* rf^C ' ^^ I Jr 1 i^-
l>i 'i L ' " ^. Jr^ i fc ^v ^r \. *\.
' " ' T-TT ! L.r 11 11!! ! ! ! % J rT 1 ^MMN
oc _ ^ : \ H
1 K a ■ J - - -j- 5 - J rx _.L_ _ ■:: i^ o tX-- -'_ . .5. f« .: :_: rX - - ^ ?»_ : Jr fx. _ __>^ >f*;::..::. ^ :: ::::*:i-: in: S 5-— 3 w**\ 1' r—:::::::":-4:
2fe: + :::III:I:: :: _ _ _ -. - ■ j - - - t- \ 5
L ^»j, ^
^ \
s. { V , ' - ■ J c 1 \ s : . \ c------------
_ x ___. \ ;-__4_:J s::
V s .1,
!r .1,
^r 5: ^^,
20- x ::: Jiiv 0 50 100 150 200 250 J3
TIME, MILLISEC
FIG. 19- Loads Experienced by Aircraft Under Fast Salvo Ejection Utilizing an Aero 7A Rack, and 195Tb Canisters.
IA
— NAVWKPS REPORT 8439
j ^ mount 1
<*■ __—+—TENSION CELLS ,
^^ T r COMf-flESSfON CELLS
OlSCENStH
A-A
b'iG. /.0. Ejection Load Test Setup.
I'he Gladeyc inte rvalomete r provideu a «ingle-fire capability au well au three «alvu muden. TheBe aalvo rnode« provide for a delay Ijetween (aniuterN of 5Ü. 100, and 300 IDB. The intervalometer current requirement between firing pulse« i« 3. 0 ampere« in «alvo modes. It i« dcuigned uo a« not to draw any current during cartridge firing. The output pulae from the intervalometer to each ejector is approxi- mately / 1 IM:, long. Current test data indicate that reliable cartridge ignition of both cartridge« for thi« pul«e width require« 12. ampere«.
<>5
NAVWEPS REPORT 8439
FIG. 21. Gladeye Dispenser Wiring Diagram and Inter
-(/ Z 3 * J 6 7 9 9/0 // //}- — t—I 1 ' ' 1 ' ' 1 1 ' r-'
r*4
— !
Q tfysc ro/rs
. t/weis ontmwjtf jcyiesmw *sss-ir-«vcf
iT ^T, ^^ -^# MKMRV ''ö JITJOStfimV
3. f^zcr&r ^w.^vz. Avov-of t*arr .**&&/ &&** syscrar <r/9/erle/0&s3
TIG. 21. Gladeye Dispenser Wiring Diagrana and Intervalometer Schematic.
INITIAL DISTRIBUTION
11 Chief, Bureau of Naval Weapons RMMO (1) RMMO-2 (I) RMMO-3 (1) RMMO-4 (1) RMMO-43 (3) RMMP-4 (1) RSWI-2 (1) RSWI-5 (1) RSWI-6 (1)
DLI-31 (2) RAAD-13 (I) RAAV-3 (1 ) RAAV-4 (1) RM-12 (1) RM-3 (1 ) RM-33 (I) RM-377 (I) RM-379 (1 )
3 Chief of Naval Operations OP-55 (I) OP-72 (1) Operations Evaluation Group (1)
1 Air Development Squadron 5, China Project Officer)
1 Naval Air Engineering Facility (SI), Philadelphia
1 Naval Air Test Center, Patuxent River 2 Naval Weapons Services Office 3 Air Proving Ground Center, Eglin Air Force Base
Detachment 4, ASD (1) PGAPI (2)
1 Air University Library, Maxwell Air Force Base 10 Defense Documentation Center (TISIA-I )
2 Douglas Aircraft Company, Inc. , Long Beach G. Ruyter (1 )
1 Grumman Aircraft Engineering Corporation, Bethpage, N. Y. 1 Lockheed Aircraft Corporation, Burbank, Calif. (Aircraft Ordnance
Group) 1 McDonnell Aircraft Corporation, St. Louis (Ordnance Division,
V. M. Marti) 1 Vought Aeronautics, Dallas
Lake (Conventional Weapons
Naval Air Engineering Center,
NOTS CL 77t (l/a4) 110
