View allAll Photos Tagged exploding

80 degree dewpoint = BOOM!

Grand Teton National Park

 

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These photos show the fiber optic sprays and color-changing LEDs that can be added onto the color-changing/fireworks kit to simulate exploding firework shells.

Equally Stupid´s "Exploding Head" ablum artwork.

Design by Espen Aeng and Kim Holm

This was one of the HiJinx setups at the photography conference I went to this past weekend. The balloon was filled with corn starch and when popped, it set off a sound trigger that was hooked up to a strobe. Yes it’s been done before, but it was still fun to do in person =)

A storm filled sky explodes in color at sunset above a water tower in Silver Creek near Park City, Utah. (c) 2011 Tom Kelly

Bored at the Jacob Javits Convention Center, NYC. More manual zoom.

I said I would sporadically post more shots from that great storm at Porthleven, and here is one. This time shot with the 17-40mm lens. I liked the light in this one, and that exploding plume of water. I felt it caught the energy involved and the wide angle captures a sense of scale and context.

This particular wave actually went higher still but went into a thin whispy shape and lost its form, so I stuck with this. It is worth noting this wave covers a huge 3 story house behind it, set high up on the cliff. I don't know how tall this is but the houses on the left look especially small. They must be 30ft approx so work it out!

Anyways, I hope you like it and thanks for your comments and faves, I really appreciate it.

 

Exposure: 0.01 sec (1/100)

Aperture: f/11.0

Focal Length: 33 mm

ISO Speed: 100

Exposure Bias: +1/3 EV

 

www.joerainbowphotography.com

 

View On Black for best results!

Orange and Almond cake with Chocolate Ganache. Please ignore lighting as this pic was taken at 6am

www.facebook.com/pages/Love-of-Cake-by-Kelly-Casey/194277...

Taken with a MAKE high speed flash trigger.

 

It's basically a firework inside a Rose, most of the stuff you can see coming out on the right is the fuse burning down (should have cut it shorter). Also the firework wasn't really inside the rose, more shoved towards the back of it - to really blow it apart I'd have had to bore a little hole for, but I'd made enough mess by the time I realised this.

 

Has given me some ideas for future shots though. There's just so many things to blow up!

 

Blog: www.photosmudger.com/

 

www.tmphoto.co.uk/

Setup for Eruption followed Ryan Taylor's excellent Water Figure Tutorial.

 

I forgot to shoot the setup at the time so I have recreated it.

 

Out of picture, my pc is running Multisine 1.74. Using the headphone output I have then connected my pc via the Mic input to an old stereo (at the the top of the picture) which is connected to the speaker.

 

The speaker was wrapped in clingfilm, and a small amount of a 50:50 cornflour (cornstarch)-water mix was placed on top.

 

Due to the small space, I could not get the legs of my Giottos MTL9361B tripod splayed wide enough to drop the camera in line with the top of the speaker. So I moved the centre column into the lateral position and hund the camera upside down off my Manfrotto 322RC2 ball head.

 

The lights on the landing and bedroom behind were turned off and at f/16 I ran a 5 second exposure. Using my wireless remote shutter I triggered the camera. During the 5 second exposure I activated a 0.2 sec pulse at a frequency of 120Hz on my pc and using a PT-04 wireless flash trigger in the other hand tried to time the flash to coincide with the sound. This took several attempts to time it right, and in actual fact the final Eruption shot is actually a blend in CS3 of two images in order to increase the drama.

 

The ghosting in Eruption is not an artefact of blending the two images, but due to some double triggering of the flashes when I pressed the remote trigger.

 

The pink/orange hues in the conflour-water mix of the final shot are, I think, attributable to the flashes bouncing off the bare plaster walls. This was not intended but presumably it would have helped to soften the light as specular highlights are not too much of a problem.

 

The final edit involved usual adjustments in LR3.6 to saturation, levels, sharpening etc together with burning in CS3 to darken the background which in the original shot I felt was distracting.

    

Olympus XZ-1

1/15 sec at f/1.8

ISO 200

6 mm

Copyright 2011 Ben Gethin

Experiments with a bb gun and strobe. The timing is complicated so I used my intervalometer to automatically fire the camera and strobe every second. The rest was all timing and Luck.

 

If you look closely, you can prob see the entry and exit stream from the bb, btw, I have Excellent aim-I should've been a sharpshooter ;)

 

I used an air rifle, water balloon, rubber band, an intervalometer, 70-200mm lens, 2 800ws heads and my lovely 50D.

Exif info:

ISO Speed rating: 100

Focal Length: 100mm

Aperture: f/8

Shutter Speed: 1/200 of a second

Lens: EF 100mm f/2.8 Macro USM

Model: Canon 5D MK II

Flash: Did fire

Flash Type: Speedlite 580EX II

Another blown up Chinese battery, this time in my Verizon Moto E4 plus. Notice the lack of UL certification.

Still this awesome sunset from Nordnesparken, Bergen.

 

Sigma 10-20 w/circular polarizer, 8 sec, f/22

 

View Large On Black - really : )

Handheld fireworks shots before deepavali nights in Brickfields, KL

Couldn't really slow down our video camera enough to capture this correctly.

Hyperion, Hypersonic Mach 15 Scramjet Missile - IO Aircraft - ARRW, HAWC, Air Launched Rapid Response Weapon

Length: 120" / Span 25"

www.ioaircraft.com

 

Scramjet, Hypersonic, ARRW, HAWC, Air Launched Rapid Response Weapon, Scramjet Physics, Scramjet Engineering, Hypersonic Missile, hypersonic weapon, hypersonic fighter, hypersonic fighter plane, tgv, tactical glide vehicle, hypersonic commercial aircraft, hypersonic commercial plane, hypersonic aircraft, hypersonic plane, hypersonic airline, tbcc, glide breaker, fighter plane, hypersonic fighter, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, boost glide, tactical glide vehicle, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, defense science, missile defense agency, aerospike, hydrogen aircraft, airlines, military, physics, airline, aerion supersonic, aerion, spike aerospace, boom supersonic, , darpa, onr, navair, afrl, air force research lab, office of naval research, defense advanced research project agency, afosr, socom, arl, army future command, mda, missile defense agenci, dia, defense intelligence agency, Air Force Office of Scientific Research,

 

Iteration V8, Hyperion Mach 15 #hypersonic #scramjet (50% faster then the X-43 #nasa), 300% faster than #Lockheed, #NorthropGrumman, #Raytheon, and Boeing. Much is sanitized as the technology advances are dramatic and not public.

DOD's funding of #AGM-183A / Air Launched Rapid Response Weapon, the poeple developing it barely comprehend student level capabilities and 50/50 it will disintegrate even at Mach 5. China and Russia, already much faster and higher tech making it obsolete already, India's recent test, apx 700 mph faster.

 

Summarized details are accurate

#hypersonic #hypersonics #scramjet #hypersonicplane #hypersonicaircraft #skunkworks #spaceplane #boeing #lockheed #raytheon #bae #bombardier #airbus #northopgrumman #generaldynamics #utc #ge #afrl #onr #afosr #ReactionEngines #spacex #virginorbit #usaf #darpa #mda #rollsroyce #nasa #tesla #safran #embraer #AirLaunchedRapidResponseWeapon #additivemanufacturing #military #physics #3dprinting #supersonic #ramjet #tbcc #collinsaerospace #rockwell #phantomworks #hypersonicmissile #alrrw #boeingphantomworks #generalatomics #cessna #dassault #arl #unitedlaunchalliance #spaceshipcompany #navair #diu #dia #usaf #unitedtechnologies #defenseadvancedresearchprojectagency #graphene #additivemanufacturing

 

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Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.

 

Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.

 

Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.

 

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Advanced Additive Manufacturing for Hypersonic Aircraft

 

Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.

 

Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.

 

*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.

 

What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.

 

Unified Turbine Based Combined Cycle (U-TBCC)

 

To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5

 

However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.

 

Enhanced Dynamic Cavitation

 

Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.

 

Dynamic Scramjet Ignition Processes

 

For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.

 

Hydrogen vs Kerosene Fuel Sources

 

Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.

 

Conforming High Pressure Tank Technology for CNG and H2.

 

As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.

 

As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).

 

Enhanced Fuel Mixture During Shock Train Interaction

 

Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.

 

Improved Bow Shock Interaction

 

Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.

 

6,000+ Fahrenheit Thermal Resistance

 

To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.

  

*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope

 

Scramjet Propulsion Side Wall Cooling

 

With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.

 

Lower Threshold for Hypersonic Ignition

 

Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.

 

Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities

 

Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.

 

Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)

 

To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.

 

A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.

 

It was a balloon...

 

CONTAX G1 + Carl Zeiss Biogon 28mm F2.8

 

 

A tiring night of watching an amazing fireworks competition. Here's a capture of the night's events with my iPhone 4.

mushrooms explode (burst) through the asphalt.

Another image with a painted effect added to it.

Another paper-pieced star from quilterscache.com!

I took this picture out my back door on June 10th, being the peak of the stormy season this year, while the storms that blew through threatened us frequently with hailstorms, thunder and lightning storms, and and even tornadoes among the many windstorms. Among all of these threats, spring decided to jump into full swing, making everything that grows around here more green, lush, and colorful than ever I remember it being and lasting longer than I ever remember it doing so before.

 

Amid the many rain and hail showers along with a tornado watch on this particular day, if I remember right, I caught this amazing storm cloud display. The sun rays were just shooting through it in an explosive fashion though the sun was clear across the other side of the sky. Since I had to piece together four pictures to get this one--because I don't have a wide angle lens at this time--some of this storm cloud's spectacular illumination and definition of the sun rays have faded. However the overall effect of the picture, I think, was captured.

 

When I played around with it in one of my graphics programs, I even found that when I changed the color of it to red, it actually looked like a huge bomb exploding. It is in these moments of nature's massive displays of power, that I am reminded of God's all-surpassing power, a power that far exceeds even any of these kinds of storms on earth or in this solar system, let alone in the entire universe.

 

As this realization sweeps over me, it evokes a kind of awe and wonder at who and what He must really be... Within my heart, while in this state, I ask His many critics this: Is it then too wonderful to imagine that in His might, He could stoop down and bless us with a portion of Himself in Jesus His Only Begotten Son through a virgin in all holiness so that we could live with Him in Eternity because His love for us is more explosively powerful than any power display in nature? No, it is not too wonderful to imagine...

 

Some imagined atheists may claim that this way of looking at God is too simplistic, that the universe displaying its power speaks of itself, not God, that it is eternal. My reply to that is nothing in the universe is eternal and in fact ALWAYS decays; therefore, it cannot be eternal. It instead is decaying. Truth be told, linear time and a decaying creation can only exist if there is such a thing as eternity. It all had to start somewhere with linear time and creation but not so in eternity where there is no beginning or end thus no decay since decay has an end.

 

Atheists are free to "believe" in the universe if they please, but it makes them, then, not atheists but rather universe worshipers. And I would much rather "believe" in One who showed His massive power by sending His Only Begotten Son because He loves me personally so that I too can live with Him in eternity than "believe" in an impersonal universe that displays its power for obviously narcissistic purposes alone.

 

As a result, though these kinds of power displays in nature can sadly bring heartache and trouble to many, I sometimes find myself actually gaining faith in more of the Only Eternal One's abilities when I look at them from a distance, catching a rare glimpse at the whole picture in the midst of these exploding storm clouds.

 

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Here are some passages that spoke to me about what I was looking at in this picture and about what I was feeling regarding it all:

  

I love you, O LORD, my strength.

 

The LORD is my rock, my fortress and my deliverer;

my God is my rock, in whom I take refuge.

He is my shield and the horn [a] of my salvation, my stronghold.

 

I call to the LORD, who is worthy of praise,

and I am saved from my enemies.

 

The cords of death entangled me;

the torrents of destruction overwhelmed me.

 

The cords of the grave [b] coiled around me;

the snares of death confronted me.

 

In my distress I called to the LORD;

I cried to my God for help.

From his temple he heard my voice;

my cry came before him, into his ears.

 

The earth trembled and quaked,

and the foundations of the mountains shook;

they trembled because he was angry.

 

Smoke rose from his nostrils;

consuming fire came from his mouth,

burning coals blazed out of it.

 

He parted the heavens and came down;

dark clouds were under his feet.

 

He mounted the cherubim and flew;

he soared on the wings of the wind.

 

He made darkness his covering, his canopy around him—

the dark rain clouds of the sky.

 

Out of the brightness of his presence clouds advanced,

with hailstones and bolts of lightning.

 

The LORD thundered from heaven;

the voice of the Most High resounded.

 

He shot his arrows and scattered the enemies ,

great bolts of lightning and routed them.

 

The valleys of the sea were exposed

and the foundations of the earth laid bare

at your rebuke, O LORD,

at the blast of breath from your nostrils.

 

He reached down from on high and took hold of me;

he drew me out of deep waters.

 

He rescued me from my powerful enemy,

from my foes, who were too strong for me.

 

They confronted me in the day of my disaster,

but the LORD was my support.

 

He brought me out into a spacious place;

he rescued me because he delighted in me. (Psalm 18:1-19, NIV)

 

Here is another passage that others have wonderfully recently connected to the Star of Bethlehem regarding Jesus' birth. But as C.S. Lewis said, there are many different levels of understanding and applying Scripture because it is divine. To say that any passage only has one meaning is immature and puts the person doing the dictating of the meaning in a place of too much power and thus is not to be trusted. However, there is such a thing as "error" such as salvation through works instead of through grace, not in keeping with the whole picture of Scripture. Keeping that in mind, here is the passage I believe relates well to what I was saying though obviously is just another level of understanding Scripture:

 

The heavens declare the glory of God;

the skies proclaim the work of his hands.

 

Day after day they pour forth speech;

night after night they display knowledge.

 

There is no speech or language

where their voice is not heard.

 

Their voice goes out into all the earth,

their words to the ends of the world.

 

In the heavens he has pitched a tent for the sun,

which is like a bridegroom coming forth from his pavilion,

like a champion rejoicing to run his course.

 

It rises at one end of the heavens

and makes its circuit to the other;

nothing is hidden from its heat. (Psalm 19:1-6, NIV)

Delicious, Refreshing…

 

View blog: bryanlawler.com/bl/exploding-coke

 

Photo by: Bryan S. Lawler

Web site: www.bryanlawler.com

Must be viewed large to see the detail

Hallowe'en themed model shoot at Exposure Studios

Colored pencil, Marker, and Crayon on Paper

 

11.5" x 15"

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