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Read why the catastrophe in the sky was also a disaster in the newsroom. |
It's the 25th anniversary of the Challenger disaster. This was an event so shocking, so unexpected, so emotionally intense that most of us still can recall that day with rare clarity. Today I am linking to an earlier post that examined the disaster and why newspapers around the world had disasters of their own when it came to running the picture of the shuttle disintegrating high in the sky off Florida.
The linked post was inspired by an editorial by Paul Berton the former editor-in-chief of The London Free Press:
Catastrophe in the sky.
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As to the question of did or didn't Challenger explode, the following is from the Huffington Post comments accompanying the
Huffington Post article on the 25th anniversary of the disaster. As you can see, the argument continues 25 years later.
After reading the comments below, it's worth noting that Challenger did not explode.
A jet of hot gas leaking from the aft segment joint of the right solid rocket booster burned through the aft attach strut between the SRB and the external tank. When the aft end of the SRB swung loose from tank, it drove the tank and orbiter into the oncoming airstream at a high angle of attack.
Aerodynamic loads caused the near-immediate structural failure of the external tank, releasing a massive plume of hydrogen and oxygen that ignited in the wake of the left SRB. This is called deflagration, which differs from detonation in that the propagation of the flame front is subsonic.
The rest of the vehicle, including the wings and vertical stabilizer of the orbiter, proceeded to break up due to the aero loads, but the crew compartment -- which is a self-contained pressure vessel attached to the airframe at four points -- was flung from the vehicle and remained structurally intact until it crashed into the ocean at over 200 mph.
Three of the four Personal Egress Air Peaks (PEAPs) on the flight deck were activated and exhibited air consumption consistent with the 2:45 ballistic trajectory between breakup and crash. These packs provide unpressurized air and would not have kept the crewmembers alive if the crew compartment had lost pressure integrity at over 60,000 feet in altitude.
Additionally, several lever-locked switches on the pilot's right-hand electrical power system control panel were thrown after the loss of telemetry downlink, which indicates a futile attempt to restore power to the crew compartment (which had ripped free of its connections to the fuel cells).
Even if the crew had been equipped with full-pressure ACES suits and parachutes as they are today, it is unlikely that they would have been able to successfully bail out the crew compartment on a free-fall ballistic trajectory. The emergency egress system designed in the aftermath requires that the orbiter is in stable controlled flight (but will not be able to make a safe landing).
The only thing that could have saved them would have been a parachute system for the whole crew compartment, similar to those equipped on the F-111 fighter-bomber. This was rejected, ironically, because of the perceived cost and complexity of separating the crew compartment from the vehicle, when Challenger plainly demonstrated that the crew compartment is quite capable of being flung free of the vehicle in the event of a complete aerodynamic breakup.
A jet of hot gas leaking from the aft segment joint of the right solid rocket booster burned through the aft attach strut between the SRB and the external tank. When the aft end of the SRB swung loose from tank, it drove the tank and orbiter into the oncoming airstream at a high angle of attack.
Aerodynami
The rest of the vehicle, including the wings and vertical stabilizer of the orbiter, proceeded to break up due to the aero loads, but the crew compartmen
Three of the four Personal Egress Air Peaks (PEAPs) on the flight deck were activated and exhibited air consumptio
Additional
Even if the crew had been equipped with full-press
The only thing that could have saved them would have been a parachute system for the whole crew compartmen