fig1 is a side view of the present invention , a modular display assembly 30 . as can be seen , the modular display assembly 30 has a first frame 2 with a first opening , a window 14 , a second frame 4 with a second opening , a plurality of light emitting diodes 18 mounted on a circuit board 8 and a base plate 16 . it is contemplated that by mounting the light emitting diodes 18 on the circuit board 8 instead of having them be two separate components , space and costs could be saved . by mounting the light emitting diodes 18 on the circuit board 8 , space requirements are reduced , because there will be only one component instead of two . thus , the width “ w ” of the modular display assembly 30 will be reduced . furthermore , it will cost less to manufacture light emitting diodes 18 mounted on a circuit board 8 because there is only a need to produce one component instead of two separate components . a cots light emitting or transmitting display subassembly 6 such as a liquid crystal display can be attached to the second frame 4 . as can be seen , the first frame 2 is attached to the base plate 16 to form a cavity 28 . a window 14 is attached to the first frame 2 at the first opening for enclosing the cavity 28 . the first frame 2 may be made of metal , glass , plastic , or a combination thereof , such as a metal coated glass filled plastic . the first frame 2 is preferably electrically and thermally conductive , and relatively impact resistant . the base plate 16 is also electrically and thermally conductive , and be relatively impact resistant . the window 14 is preferably made of glass layer 10 . the window 14 could also have a conductive indium tin oxide layer ( not shown ). the window 14 could be made of other materials , such as those disclosed in saxena et al . ( u . s . pat . no . 7 , 167 , 309 ). the window 14 is preferably electrically and thermally conductive , and also relatively impact resistant . adjacent the window 14 is an indium tin oxide layer heater and electromagnetic interference ( emi ) shield 22 . because the first frame 2 , the window 14 , and the base plate 16 are electrically conductive , they could form a faraday cage around the cots light emitting or transmitting display subassembly 6 . this protects the cots light emitting or transmitting display subassembly 6 from electromagnetic or other types of interference and the display assembly from emitting electromagnetic or other types of interference . because the first frame 2 , the base plate 16 , the window 14 are relatively impact resistant , the structure will prevent damage to the cots light emitting or transmitting display subassembly 6 . furthermore , the first frame 2 , the window 14 , and the base plate 16 are preferably sealed to protect the cots light emitting or transmitting display subassembly 6 from humidity , salt fog , and harmful particles such as sand , rocks , debris , or dust . diffusers and / or film 26 could be located between the cots light emitting or transmitting display subassembly 6 and the light emitting diodes 18 . the present invention contemplates that drive electronics 12 for driving the cots light emitting or transmitting display subassembly 6 is located in the cavity adjacent any one of the sides of the circuit board 8 adjacent to the base plate 6 . the base plate 16 works in conjunction with the first frame 2 and the window 14 to maintain the drive electronics 12 , circuit board 8 , light emitting diodes 18 , diffusers and / or film 26 , the cots light emitting or transmitting display subassembly 6 , second frame 12 relatively immobile during shock and vibration . the second frame 4 is adjacent to the drive electronics 12 . the second frame 4 works in conjunction with the first frame 2 and window 14 to maintain the drive electronics 12 , circuit board 8 , light emitting diodes 18 , diffusers and / or film 26 , and the cots light emitting or transmitting display subassembly 6 in a relatively immobile state during shock and vibration . the second frame 4 works in conjunction with first frame 2 and the base plate 16 to maintain the drive electronics 12 , circuit board 8 , light emitting diodes 18 , diffusers and / or film 26 , the cots light emitting or transmitting display subassembly 6 in a relatively immobile state during shock and vibration . the present invention prevents the cots light emitting or transmitting display subassembly 6 from being damaged by reducing the likelihood that the components contained within the modular display assembly 30 , such as drive electronics 12 , circuit board 8 , light emitting diodes 18 , diffusers and / or film 26 , the cots light emitting or transmitting display subassembly 6 will move around in the cavity 28 . the modular display assembly is mounted , for example , on a customer bulkhead 24 , such as on an airplane , a helicopter , a tank , a car , a boat , a bunker , for example . the modular display assembly 30 preferably also has a bezel and controls 20 to allow a user to control the cots light emitting or transmitting display subassembly 6 , such as brightness and contrast . there could also be an optional connector and electromagnetic interference filter 40 connected to the base plate 16 and the circuit board 8 . fig2 is an exploded side view of the present invention while fig3 is an exploded perspective view of the present invention . as can be seen , the modular display assembly 30 has a window 14 , a first frame 2 , a second frame 4 , diffusers and / or film 26 , a cots light emitting or transmitting display subassembly 6 , a plurality of light emitting diodes 18 mounted on a circuit board 8 , and a base plate 16 in a sandwich structure . as shown in fig3 , the modular display assembly 30 has a height “ h ,” a length “ l ” and a width “ w .” the three axis of the display assembly 30 related to the dimensions by the x axis being parallel to the width “ w ,” the z axis being parallel to the height “ h ,” and the y axis being parallel to the length “ l .” fig4 is a chart detailing input for testing successfully performed on two samples of the present invention . these samples of the present invention were tested for four hours , fully operational , on each axis x , y , and z with each axis x , y , and z in turn being parallel to the ground . for example , four hours of operational testing was done with the axis x parallel to the ground . four hours of operational testing was done with the y axis parallel to the ground . four operational hours of testing was done with the z axis parallel to the ground . both samples of the present invention met all operational requirements , without damage , throughout the 12 total hours of testing . in each of the 4 hours of testing for each axis , one hour was spent meeting the mil - std - 810 vibration requirements of the h - 1 cobra helicopter , including gunfire vibration 32 , one hour was spent meeting the endurance vibration requirements of the e - 2d hawkeye carrier bound aircraft 34 , one hour was spent meeting the functional vibration requirements of the e - 2d hawkeye carrier bound aircraft 36 , and one hour was spent meeting the endurance vibration requirements of the mh - 60 helicopter 38 . as can be seen in fig4 , the chart summarizes and compares the random vibration requirement for the 3 avionics platforms , and presents frequency ( hz ) vs . power spectral density ( psd ) in g 2 / hz where g is the force of gravity ( approx . 9 . 80665 m / s 2 or approx . 32 . 174 ft / s 2 ) for each test that the present invention was subjected to . the present invention had no anomalies or performance issues such as flicker for the 4 hours of testing on each axis x , y , and z . furthermore , the two samples of the modular display assembly 30 were also subjected to 20 functional shocks and 40 crash safety shocks . there were no anomalies or performance issues such as flicker in the present invention during these tests .