US1337566A - Flash-gun - Google Patents

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US1337566A
US1337566A US334792A US33479219A US1337566A US 1337566 A US1337566 A US 1337566A US 334792 A US334792 A US 334792A US 33479219 A US33479219 A US 33479219A US 1337566 A US1337566 A US 1337566A
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chamber
gun
charge
flash
oxygen
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US334792A
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Raymond C Pierce
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A33/00Adaptations for training; Gun simulators
    • F41A33/04Acoustical simulation of gun fire, e.g. by pyrotechnic means

Description

R. C. PIERCE.
FLASH GUN.
APPLICATION FILED OCT. 3l. l9l9.
Patented Apr. 20, i920.
3 SHEETS-SHEET I.
R. C. PIERCE.
PLAS-H GUN.
APPLICATION FILED OCT. 3l. i919.
PatentedvApr. 20, 1920.
3 SHEETS-SHEEI 2.
. n. c. MERCE.`
FLASH GUN. APPLICATION FILED. O CT. 3l 1939.
Patented A 3 SHEET' 293s r1 9206 TS-SH RAYMOND C. PIERCE, 0F HOB-NELL, NEV YORK.
FLASH-GUN.
Application filed October 31, 1919. Serial No. 334,792.
(FILED Umane THE Aer or Manon s, 1883, 22 STAT. L., c25.)
To all whom t may concern.'
Be it known that l, RAYMONDl C. PIERCE, captain, Air Service, Military Aeronautics, a citizen of the United States, and residing at Hornell, in the county of Steuben and State of New York, have invented an Improvement in Flash-Guns, of which the following is a specification.
The invention described herein may be used by the Government, or any of its oflicers oremployees in prosecution of work for the Government, or by any other person in the United States, witho-ut payment of any royalty thereon.
The present invention relates to devices for producing flashes by the ignition of combustible substances, and more particularly to a flash gun capable of simulating artillery fire. v
One object of this invention is to provide a device which may be used to create a flash similar to that of a cannon, howitzer, etc.
A second object is to furnish a' device of the class described, which shall be capable of use 'in the training of aerial observers in the observation of artillery lire. It will be understood that aerial observers in actual warfare are stationed either above or near the front lines in airplanes or balloons, from which they take charge of the fire of artillery batteries observing the eflect of the fire as indicated by the flashes of the exploding shells.
In the training of aerial artillery observers, battle conditions I are duplicated as nearly as possible but it has been found impracticable, Vin many instances, las well as expensive, to train observers by the firing of loaded shells, and attempts have been made to produce a device, which may be used t0 create a flash similar to that of artillery. Previous experiments have developed appliances using smokeless powder, as the combustible substance. but smokeless powder has numerous disadvantages in use, being dangerous to handle. Furthermore, a flash gun using powder can not be recharged with rapidity and it is necessary for the operator to remain in proximity to the gun while in operation.
A further object of the invention then is to furnish a means of producing a flash,
which Shall be Capable ef. rapid manipuletion and which may be operated from a distance. A
To attain this' end, it is contemplated to employ a liquid or gas as the combustible substance and'to permit of remote control to employ electrical controlling and ignition devices. To create a flash resembling artillery it has been found best to mix the combustible with oxygen under pressure and a mixture of gasolene and oxygen furnishes a satisfactory combination.
Another object of the invention, then, is to produce a device in which the mixture of the ingredients may be effected and controlled yfrom a distance. This permits the operator to remain in a position of safety and serves further ends, as will be shown. Remote control of the gun together with automatic functioning of the parts permits of the use of the gun in a number of useful applications. lt may be used, for instance, to deceive the enemy as to a true gun position. By firing the flash gun located at a distance from the lbattery simultaneouslywith the'battery guns, where the simulation is nearly perfect as in this case, the enemy is unable to determine by observation what the true gun position is. Then a battery is to be moved, flash guns may be left behind and by means of the remote control, it is possible to operate the gun in safety to imitate the artillery battery and conceal the fact of the removal.
In connection further with the use of this device for camouflage purposes, the present gun has another valuable characteristic, in that in operation the report caused by the firing of a charge can hardly be distinguished from that ofthe ordinary 3 field piece. In modern warfare it should be understood that the locationof batteries is accomplished not only by actual observation of the flash, but also by the noise of the report. rlhis means of location depends upon the use of sound ranging devices which have recently been developed to a highstate of proficiency. With this gun, then, which simulates actual artillery not only as to Hash, but also as to report, it will be .seen that its use in the field is of the utmost advantage. Vith the gun herein described and shown, the report is similar to that of a light field piece, but by a slight modification-of the parts, such as the increase in the aperture of the igni' tion chamber and the use of a larger charge of combustible material, artillery of different sizes may be so closely imitated,both as to appearance and report of discharge, as to deceive observers using both visual and auditory means of observation.
Briefly stated the flash gun forming the subject matter of the present invention depends for its effect upon the projection into the atmosphere ofia volume of ignited gas. llVhile ignition takes place within the gun, the combustion occurs in the atmosphere, and in this way any explosive effect is eliminated. A further point of novelty is that the'combust'ible is not ignited continuously to produce a flame, but is fed into the ignition chamber in individual charges, each of which is used to produce a flash. Combustibles have been used alone and in combination with compressed gases to propel projectiles -and for this purpose the combustible -is employed in the form of a definite charge vintroduced into the ignition chamber. Combustibleshave also been used, as in lflame-throwing devices', for instance, in combination with Vcompressed gases to produce a jet of flaming material. ln such cases the combustible is fed continuously from the container. But in the flash gun here described, though ignition occurs within the gun, the combustion takes place in the atmosphere and there is projected from the gun a mass of burning gas.
Furthermore, the flash occurs as the result of the combustion of a definite charge of combustible, fed intermittently and at will into the ignitionl chamber. The burning `of the charge taking place outside of the gun eliminates such an explosive effect as. would occur `where the use is that of a propellant.
length but in color and visibility. In the present Hash gun, the variation is veasily accomplished by changing the proportions of the fuel and the oxygen in the mixture, and also by changing the pressure at which the oxygen is stored.
' Still another object of the invention is te produce a device which shall be inexpensive to manufacture, simple in operation,j light in weight and durable in use. Obviously, a flash gun in use in the field is likely to draw enemy fire and it is essential that it should be cheap to construct.;y Simplicity of operation is necessary as the gun has to withstand rough usage and it is necessary that' it should not fail. The present invention provides a flash gun which has the above will appear from time to time in the followj ing description and claims, for a better understanding of the invention reference is made to the accompanying drawing embodying a preferred form of the device.
Referring now to the drawings:
Figure l is a side view of the liash gun in operative position;
Fig. 2 is a view. in elevation of the rear end of the gun;
Fig. 8 is a view in elevation of the front end of the gun; A Y
Fig. 4L is a view in cross section of the oxygen control mechanism located at the lfront end of the gun;
Fig. 5 is a view partly in cross theL new form of float valve;
Fig. 6 is a view in side elevation, with parts cut away, of a spring weighted swing check valve;
Fig. 7 is a plan view of the diaphragm used in the oxygen control valve;
Fig. 8 is a plan View of a bushing used iin connection with diaphragm` shown on F ig. 7;
Fig. 9 is a view in longitudinal section of the gasolene check valve;
Fig. 10 is a diagram of the electrical connections.
The invention may be briefly described as consisting of a pair of tanks to contain oxygen and lgasolene respectively, electrically controlled devices to release and mix the ingredients, a chamber inA which the charge is to be ignited, and electric ignition mea-ns.
The oxygen is contained in a cylindrical container designated as l and located alongside of this container is a similar reservoir 2 in which the gasolene is stored. The oxygen is introduced into the container through a valve 3 from the tanks of highl compressed gas at a pressure of approximately pounds per inch through a pressure reduction valve. Gasolene is introduced into the reservoir 2 through an opening provided with a screw threaded cap member 4. The gasolene is under atmospheric pressure.
Referring now to Fig. 4 there is located within the container l a longitudinal pipe 5, one end of which projects through a bushing or collar 6 in the forward end of the reservoir l. Bushing 6 is provided with a series of longitudinal holes 7 drilled through the body thereof, and an annular channel 8 is cut in the face of bushing 6 so as to connect the holes 7. Forming the outer edge of the channel 8 is a shoulder 9 on the face of the bushing, within which rests a diaphragm 10. rllhis may be of some form of rubber packing and is shown in Fig. 4. This diaphragm rests within the shoulder so as to cover the channel 8, thus closing the holes 7.
A bonnet 11 fits against the face of the section of diaphragm 10 and is held in place by a bar 12 and bolts 13 with lock nuts 14:. As seen in Fig. 3 these bolts are secured in the end of the reservoir 1. lVithin the bonnet 11 is a chamber 15 slightly larger in diameter than the v'pipe 5 and located in the chamber is a spiral spring 16 holding a plunger 17 against the face of the diaphragm. The inner edge of the bonnet is beveled as shown at 18 for a purpose to be later described. Drilled through the diaphragm and registering with one of the Vholes 7 is a hole 19 of small diameter.
Attached to the lower side o the bonnet l1 by a threaded connection 25 is a cylindrical container 20 within which are located the coils 21 of a solenoid. Within the solenoid and acting as a core thereoi' is a plunger 22. rlhe connection 25 has an enlarged chamber 27 in its upper end and there is provided a. passageway 28 in the shell of the bonnet connecting the bonnet chamber 15 with the chamber 2T. rlhe plunger 22 moves freely within a channel 24 in the connection 25, and diametrically through the connection 25 there are drilled passageways 2G, 26.
Located in the chamber 2T at its lower end is an annular seating 27 projecting inwardly into the'chamber 27, and surrounding the opening of the channel 24 into the chamber 27. TWithin the chamber 27 there is located a disk valve 28, provided on its lower surface with an annular projection 23a. The valve 23 seats on the seating 27 and is provided with a rubber disk- 28b mounted in its lower ace to seat the disk to make a gas tight closure.
The plunger shown, will lift the valve 23 oii" its seat when the solenoid is energized.
The operation or the oxygen control mechanism is as follows:
Vith a pressure of sixty pounds per square inch in the container 1, pressure is exerted against the diaphragm 10, the passing through the holes 7 into the channel 8. By means of the small hole 19, however, the oxygen is permitted to pass through the diaphragm and to flow into the chamber 15 in the bonnet, thus tending to equalize the pressure on both sides orn the diaphragm. The actual pressure on the bonnet side of the diaphragm is equal, however.V to the pressure of the oxygen per squarein ch, multiplier by the total area or the diaphragm, plus the pressure exerted by the-spring 16, while the actual pressure on the vother' side of the diaphragm is equal to the oxygen pressure per square inch multiplied by the area ci the annular channel. The difference is about fifty pounds pressure with a container pressure of sixty pounds per square inch.
lVhen the electrical connections are closed energizing the solenoid, the plunger 22 is moved up to displace the disk 28 from its seat. The oxygen Within the bonnet now escapes into the atmosphere through passage 28, channel 24 and passages 26. The sudden reduction'ofpressureon the bonnet side'of the diaphragm causes the diaphragm to be kdistended and forced from its seat along the edge or" the channel S. The flexibility of the diaphragm and the beveling of the inner face of the bonnet permits this distention.
With the diaphragm partially unseated a volume of oxygen now flows from the container into the pipe 5 to form an ingredient of the charge.
The solenoid is energized for an instant only, and as the plunger 22 drops when the current ceases to flow the disk valve23 is reseated, making the chamber 15 gas-tight. Oxygen now passes through the hole '19 -in the diaphragm until a suiicient pressure is built up in the chamber to reseat the diaphragm with the aid of the spring-pressed plunger 17. The reseating of the diaphragm l0 cuts oft' the flow oic oxygen from the container and the device is now ready for another shot. vItwill be seen that the amount of oxygen which is introduced through the oxygen conveying pipe into the ignition chamber may be varied in several Ways. Primarily, this is accomplished by varying the size of; the hole through the diaphragm. It the hole is made larger, the pressure of the oxygen will build up more quickly in the bonnet chamber to reseat the diaphragm. Increasing the area oi the annular channel in the face of the bushing will also serve to vary the amount of oxygen.
in a charge. 1f the area o1 the channel is increased, the oxygen Vwill exert a greater pressure on that side of the diaphragm, and it will take longer for the counteracting presssure to build up to a point where the diaphragm may be reseated. Varying the strength of the spring 16, will permit of variation in the volume of oxygen in charge. Actually, however, only the variations provided by changing the size ofthe hole in the diaphragm are employed.
At'V the rear end of the oxygen conveying,v
pipe, which projects from reservoir 1 there is a swing check valve 29 shown in Figs. 1, 2 and 6. This check valve is of the ordinary form of 'i' connection provided with a swinging gate 30 which is ordinarily held against its seat 31 by means of a sprin pressed plunger32. A Weak spring is used to actuate the plunger 32 so thatA the use of this Acheck valve does not interfere with Vthat the gate will be closed when thegas has ceased to flow' therethrough. This feallO ture is necessary to prevent the back fire from the flash traveling into the oxygen tank.
From the lower endv of the swing check valve 29 there is a pipe 33 extending downwardly and provided with a return bend so as to connect the valve with a chamber 34 placed below the reservoir and container and extending parallel to theirl longitudinal axes. This chamber is of larger diameter than the pipe 33 and it is within this chamber that the ignition of the charge occurs.
The flow of gasolene from the reservoir 2 is controlled by a float valve of the usual type but with slight modifications. The float valve is contained within the float chamber 35 which is slidably mounted on a bracket 36. The upper end of the float chamber is provided with ears 37 to one of which is attached astrap member 38 by means of a thumb screw 39. Strap-member 38 is provided with bolts 40 projecting through a slot in the bracket 36 and provided with thumb nuts 41. By means of this arrangement the float chamber' may be adjusted as to height. The second ear 37 of the float chamber is provided with a bolt 42 and thumb screw 43. Beneath the thumb screw there is a washer 44.0f large diameter. This arrangement of the parts permits the cover 45 of the float chamber to be held firmly in place along one edge while the other edge is held secure by means of strap memberV 38 which projects slightly thereover.
Connection 1s made between the float chamber and the gasolene container by means of a flexible pipe 46 provided with a shut-oil" valve 47. The pipe 46 is connected by a union to a member 48 projeeting from the top of the cover 45. Vithin the member 48 there is a sleeve 49 through which the gasolene is conveyed from the pipe 46 to the float chamber proper. The lower endvof the sleeve 49`is machined to form a seating for a needle valve. The float 50 located within the float chamber is of the usual cylindrical form provided, however, at its upper end with a stem 51 enlarged as shown at 52 to act as a needle valve, seating against the machined surface of sleeve 49. The stem 51 projects some distanceinto sleeve 49 and serves further as a guide for the float 50 in its upward and downward movement.
It will be understood thatthe gasolene flows freely into the float chamber through the pipe 46 and sleeve 49 until the level of thev gasolene in the chamber has raised the float 50 until the needle valve 52 closes the opening of the sleeve 49. In order that this closing action may be more positive and morerapid there is provided a pair of magnets diametrically placed at the top of the float chamber on either side of the sleeve 49. One of these magnets 53 is shown in Fig. 5. A thin iron disk 54 is attached to the top of the oat 50. The strength of the magnets is such that when the float 50 has been raised by the presence of gasolene in the float chamber to within a short distance of the magnets their influence on the disk 54 .raises the float 50 sharply so as to cut off the flow of gasolene. However, when the asolene has been drained from the float c amber, the weight of the float counteracts the influence of the magnets and permits the float to drop. By means of this Vmagnetic feature it is possible to measure more accurately the proportion of gasolene which is to form a part of the charge and to produce a charge more quickly. The lower end of the chamber has an outlet 55 to which is connected a flexible tube 56. Tube 56 conducts the gasolene from the float chamber to the check valve 57, for a clearer understanding of which reference is made to Fig. 9.
This gasolene check valve is made up 0f two halves 58 and 59. Gasolene is conducted from an opening 60 in the upper half through a passage way 61 to the chamber 62 formed between the halves of the valve. In the lower half there is provided a sleeve 63 forming a wall of the upper portion of the passage 64, corresponding to passage 61. The sleeve 63 projects into the chamber 62 and is provided at its projecting end with a plurality of longitudinal slots 65. Covering the end of the sleeve 63 there is a metallic diaphragm 66 of such size as to shut off 'completely the passage 61 when brought into action.
It will be seen that under ordinary conditions gasolene will flow into the check valve into the passage 61 thence into the chamber 62 and through slots 65 into the passage 64 and thence through the opening 67 which is joined by means of a connection 68 to the return bend pipe 33. It is seen that gasolene may flow freely from float chamber into the pipe 33. However, in the event of a sudden backward pressure on the gasolene the disk 66 will beforced off its seat against the end of the passage61 so as to close it completely. This arrangement is necessary and useful in preventing a back fire from entering the float chamber. The lower half of the shut-off'valve is provided with a drainagecock 67a 'of the usual type, to permit of the draining of the tube 33 and float lchamber 35 when the gun is to be taken down and stored. Y
The return bend pipe 33, as explained before, is connected at one end to the barrel 34 which is mounted between junction plates 69 and 70, located at either end of the gasolene and oxygen cylinders, and bolted thereto. These junction plates serve not only to support the barrel, but also to hold the cylinders in rigid relation. Adjacent the front end of the barrel 34: there is provided an opening for an ignition device here shown as a spark plug 71 projecting into the barrel. Beneath the gasolene container and rigidly attached thereto is a coil box 7 in which is a booster coil. A source of electrical energy, not shown, is provided and this may consist of a number of dry cells connected to the coil.
The electrical devices and connections used to fire the gun are shown in Fig. l0. A source of energy is provided, and for this purpose it is found most convenient to use a battery 76 of 6 dry cells. The source is connected on one side through a push button 77 to one binding post 78 of a solenoid 79, the other side of the battery being grounded. The other post of the solenoid is grounded as indicated at 80. In parallel with the solenoid is connected the low tension coil 8l of a booster coil 82,. which is in turn grounded as indicated at 83. The high tension coil Si is grounded on one side as shown at 85 and on the other side grounded through a spark plug 86. Vhen the circuit is closed by pushing the button 7 7 the current energizes the solenoid and starts a spark across the plug-gap at the same instant. This timing is exact enough to serve the desired purpose of igniting a charge released by the action of the solenoid on the oxygen control valve.
When it is desired to use a gun controlled from a distance it is only necessary to substitute a relay in the place of the push button, when the gun may be fired by energizing the relay to close the circuit. This actuation of the relay may, of course, be performed from any desired distance as will be readily understood.
Attached to the lower side of the barrel 3l there is a member 73 to which is pivotally and adjustably mounted a'pair of supporting legs 74. At the rear end of the barrel there is mounted a supporting leg 7 5.
When the gun is to be used in the eld the gasolene reservoir is filled and oxygen is introduced into the container at a pressure of approximately 60 pounds per square inch. The gun is set up by means of the legs forming a tripod and with the electrical connections in place it is ready for operation. As previously stated the proportion of oxygen which is to enter into a charge is determined by the size of the hole 19 in the disk l0 in the oxygen control valve and the amount of gasolene which is to enter into a charge is determined, of course, by the level of the gasolene in the float chamber. rl`he float chamber, as stated, is adjustable in its bracket and a greater or less amount of gasolene may be introduced into the return bend pipe 33 as may be desired to form part of a charge. It will be understood that gasolene will automatically flow into the pipe 33 so as to keep a certain charge continuously in the lower bend thereof. Oxygen, however, will not be 'introduced into this pipe except by energization of the solenoid actuating the oxygen control valve. lVith a charge of gasolene in the bend of pipe 33 when the solenoid is energized oxy- V gen enters the pipe 33 under pressure and at a relatively high velocity. This is sufcient to force the gasolene ahead of the oxygen into the chamber 34 and at the proper instant the spark jumps the gap in the plug igniting the charge.
Under the influence of' its initial velocity the ignited charge is projected into the atmosphere so as to produce a flash which resembles very closely that produced by artillery fire. Owing to the difference in size of the pipe 33 and chamber 34; the charge of gasolene forced from pipe 33 is partially atomized in the chamber. The charge continues forward in the chamber until ignition occurs a short distance from the end of the chamber. The heat of combustion so started is sufiicient to complete the transformation of' the charge to a volume of gas which is expelled into the atmosphere.
The visibility and appearance of the flash may be varied as may be desired by changing the proportions of the mixture. This is accomplished bv raising and lowering the float chamber. For instance, to imitate the fire of a French m/m gun a pressure of about 60 pounds of oxygen is required and a low gasolene level should be used. this resulting in a light yellow and relatively short flame. By raising` the gasolene level and using approximatelv the same pressure of oxygen it is possible to make a deep red fiame of great length which imitates very closely that produced by large howitzers. The desirability of being able to imitate flashes of different types of guns will be obvious.
It is also clear that the gun being electrically operated maybe controlled from any distance. This mav necessitate the use of relays but no considerable modification is necessary in the electrical devices themselves.
It is not desired to limit the invention to the forms shown although these are preferable, but it is clear that the various parts are capable of further modification within the meaning and scope of the appended claims.
Having thus described mv invention, what I claim as new, and desire to secure by Letters Patent is:
1. In a flash-gun, sources of fiash-producing materials. an ignition chamber having a discharge orifice, an igniter, and means to force an ingredient of a charge of said materials through the chamber to expel the ignited charge therefrom.
2. In a flash-gun, sources of flash-producing materials, an ignition chamber having a discharge orifice, an igniter, and manually controlled means for forcing one ingredient of a charge of said materials through said chamber to expel such charge ignited therein.
3. In a flash-gun, sources of flash-producing materials, an ignition chamber having a discharge orifice, an igniter, and means for forcing one ingredient of a charge of said materials through said chamber to expel such charge ignited therein.
4l. In a flash-gun, sources of Hash-producing materials, an ignition chamber having a discharge orice, an igniter, means for forcing one ingredient of a charge of said materials through said chamber to expel the ignited charge, and means to control the characteristics of the flash.
5. In a flash-gun, sources of flash-producing materials, an ignition chamber having a discharge oriice, means to vary the proportions of said materials in acharge', an igniter, and means to force an ingredient of said charge into said chamber to expel the ignited intermixture of said ingredients therefrom.
6. In a flash-gun, sources of flash-producing materials,an ignition chamber having a discharge orifice, means for controlling the admissionof one ingredient of a charge of said materials into said chamber in varying proportions, said controlling means being actuated by the passage therethrough of said ingredient, and an igniter for such charge. f
7. In a liash-gun, sources of flash-producing materials, an ignition chamber having a discharge orifice, means to control the admission of one ingredient of a charge of said materials into said chamber', means to force Va second ingredient of said charge through said chamber to expel said charge of intermingled ingredients therefrom, and an igniter for such charge.
8. In a flash-gun, sources of flash-producing materials, an ignition chamber having a discharge orifice, means to produce, a mixture of said materials in said chamber to form a charge, means to control the production of said mixture, including a valve actuated by the passage of an ingredient of said charge therethrough, and an ignited for such charge. Y
9. In a flash-gun, a source of flash-producing material, an ignition chamber having a discharge orifice, a valve to control the admission of a charge of said material into said chamber, said valve having a diaphragm seated to shut ofi' the flow of said material, means to equalize the pressure on both sides of said diaphragm, means to cause a reduction of pressure on one side of said diaphragm to cause it to be unseated, and an igniter for such charge.
l0. In a Hash-gun, comprising a source of flash-producing material, an ignition chamber and an igniter, a valve to control the admission of a charge of said material into said chamber, consisting of a bushing mounted in a container for said material, a bonnet inclosing a spring-pressed plunger, a diaphra m normally held against the face of said ushing by said plunger, means to equalize the pressure on both sides of said diaphragm, and manually controlled means to reduce the pressure on one side of said diaphragm to unseat it.
11. In a flash-gun, sources of flash-producing materials, an ignition chamber having a discharge orifice, an igniter', and means for controlling the admission of a charge of said materials into said chamber, said means being adapted to permit one ingredient of said charge to be forced through said chamber to expel the ignited intermixture of ingredients therefrom.
12. In a flash-gun, a source of flash-producing material, an ignition chamber having a discharge orifice, a valve to control the admission of a charge of said material into said chamber, said valve being partially actuated by the passage of said material therethrough, and an igniter for such charge.
13. In a flash-gun, a source of flash-producing material, an ignition chamber having a discharge orifice, a iioat valve to control the admission of a charge of said material into said chamber, said valve being actuated in part by the passage of said material therethrough and in part by magnetic means, and an igniter for such charge.
RAYMOND C. PIERCE.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4326847A (en) * 1979-12-21 1982-04-27 Mcdonnell Douglas Corporation Launch environment simulator
US4439155A (en) * 1979-12-21 1984-03-27 Mcdonnell Douglas Corporation End caps for use with a launch environment simulator process and structure
WO1996035919A1 (en) * 1995-05-10 1996-11-14 Loral Europe Limited Weapon simulator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4326847A (en) * 1979-12-21 1982-04-27 Mcdonnell Douglas Corporation Launch environment simulator
US4439155A (en) * 1979-12-21 1984-03-27 Mcdonnell Douglas Corporation End caps for use with a launch environment simulator process and structure
WO1996035919A1 (en) * 1995-05-10 1996-11-14 Loral Europe Limited Weapon simulator

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