the
Challenger Accident

Crewmembers of the STS 51-L
mission at pre-launch breakfast, January 28, 1986.
The
explosion that took the lives of the seven-member crew on board the Space
Shuttle Challenger on January 28, 1986, was one of those events that
prompt people to ask, “Where were you when…..?” Probably few peacetime
incidents have had as much impact, and few have received as much attention
from both the public as well as those involved with spaceflight, as this
tragedy has.
The
mission was planned much like many others, rather routine in fact, with
two payloads to launch and a number of experiments to be conducted on
board. Planned objectives were to launch a new communications
satellite-the Tracking and Data Relay Satellite-and flying of a module to
observe Halleys comet with two ultraviolet spectrometers and two cameras.
Other payloads were the Fluid Dynamics Experiment, the Comet Halley Active
Monitoring Program Phase Partitioning Experiment, and three Shuttle
Student Involvement Program experiments. A first-time activity was the
lesson-from-orbit that classroom teacher Christa McAuliffe planned to
teach. As well as McAuliffe, the other crew members were Francis R. Scobee,
commander; Michael J. Smith, pilot; mission specialists Judith A. Resnik,
Ellison Onizuka, and Ronald E. McNair; and non-NASA payload specialist
Gregory Jarvis, an employee of Hughes Aerospace.
The
launch, originally scheduled for January 22, had been postponed six times
because of bad weather and mechanical problems. When the decision was made
to launch, the air temperature was 36 degrees Fahrenheit (2 degrees
Celsius), cold for Florida, even in January.
Launch
finally took place at 11:38 a.m. Eastern Standard Time.

Main engine
exhaust, solid rocket booster plume and an expanding ball of
gas from the external tank is visible seconds after the
Space Shuttle Challenger accident on Jan. 28, 1986.
Photographic data later revealed that the first indication of a problem
occurred at 0.678 seconds into the flight, when a strong puff of grey
smoke spurted from the vicinity of the aft field joint on the right solid
rocket booster. The vaporized material streaming from the joint indicated
the absence of complete sealing action within the joint. Quickly,
observers saw eight distinctive puffs of increasingly blacker smoke. At
just under a minute into the flight, the first flickering flame would be
detected on image-enhanced film on the right solid rocket booster, and one
film frame later, the flame was visible without image enhancement. It
rapidly grew into a continuous, well-defined plume that was directed onto
the surface of the massive external tank, which held the fuel for the main
engines.
At 64
seconds came the first visual indication that the swirling flames from the
right solid rocket booster had breached the external tank. Within 45
milliseconds of the breach, a bright, sustained glow developed on the
black-tiled underside of the Challenger between it and the external tank.
Less than 10 seconds later, at an altitude of 46,000 feet (14,325
meters), the Challenger was totally engulfed in an explosive burn. At 73
seconds after lift-off, it exploded, claiming the crew and vehicle while
millions watched in horror on their televisions.
Moments
after the explosion, all mission data, flight records, and launch
facilities were impounded. Within an hour, NASA's associate administrator
for space flight, Jesse Moore, named an expert panel to investigate the
disaster.
On
February 3, President Ronald Reagan announced the formation of a
presidential commission to investigate the accident. The commission was
headed by former secretary of state and attorney general William P. Rogers
and consisted of persons not connected with the mission. The commission
immediately began a series of hearings that dealt with all areas of the
Space Shuttle program. In all, the commission interviewed more than 160
individuals and held more than 35 formal panel investigations, generating
almost 12,000 pages of transcript. Almost 6,300 documents, totalling more
than 122,000 pages and hundreds of photographs were examined and became
part of the commission's permanent database and archives.

Wreckage from the Space Shuttle
mission 51-L mission retrieved from the Atlantic Ocean
by a flotilla of U.S. Coast Guard and U.S. Navy vessels was returned to
the Trident Basin
at Cape Canaveral Air Force Station aboard the U.S. Coast Guard cutter
Dallas
Early in
its investigations, the commission began to learn of the troubled history
of the solid rocket motor joint and seals. Commission members discovered
the first indication that the manufacturer of the solid rocket booster,
Morton Thiokol, had initially recommended against launch the night before
because of concerns regarding the effects of the low temperature on the
joint and seal. Following further testimony, Chairman Rogers issued a
station noting that “the process [leading to the launch of Challenger] may
have been flawed.”
The
commission released its report and findings on the cause of the accident
on June 9, 1986. The consensus of the commission and participating
investigative agencies was that the loss of Challenger was caused by a
failure in the joint between the two lower segments of the right solid
rocket motor. The specific failure was the destruction of the O-ring seals
that were intended to prevent hot gases from leaking through the joint
during the propellant burn of the rocket motor. The evidence assembled by
the commission indicated that no other element of the Space Shuttle system
contributed to this failure.
In
addition to this primary cause, the commission identified a contributing
cause of the accident relating to the decision to launch. The commission
concluded that failures in communication resulted in launch decision based
on incomplete and sometimes misleading information. Further, engineering
data and management judgments conflicted and NASA's management structure
permitted internal flight safety problems to bypass key Shuttle managers.
Neither concerns regarding the low temperature and its effect on the
O-ring nor the ice that formed on the launch pad had been communicated
adequately to senior management or been given sufficient weight by those
who made the decision to launch. In addition, the heavy emphasis on
maintaining the schedule of Shuttle launches and an ambitious flight rate
diluted the resources available for a single mission and very likely
compromised quality.
The
problem with the Space Shuttle's Solid Rocket Booster joint began with its
faulty design and increased as both NASA and Thiokol management first
failed to recognize the problem, then failed to fix it, and finally
treated it as an acceptable flight risk. NASA minimized the growing
problem in its management briefings and reports, and Thiokol's stated
position was that "the condition is not desirable but is acceptable." At
no time did management either recommend a redesign of the joint or call
for the Shuttle's grounding until the problem was solved.
The
findings of the commission determined that the genesis of the Challenger
accident-the failure of the joint of the right solid rocket motor-began
with decisions made in the design of the joint and in the failure by both
Thiokol and NASA to understand and respond to facts obtained during
testing.
In its
report to the President, the commission unanimously adopted nine
recommendations. These ranged from the obvious redesign of the solid
rocket booster joints to recommendations relating to management,
communications, and safety. The commission also recommended that NASA slow
the pace of its launches. Although critical of the agency, the commission
also urged that the country continue to support NASA as a “national
resource” and applauded the agency's achievements.
At the
same time that the commission was meeting, NASA was working on defining
and implementing the actions it would take that would allow resumption of
Shuttle flights. This included redesign of the solid rocket motor that
eliminated the weakness that had led to the accident. The agency also
reviewed every element of the Shuttle system and added features to improve
safety including a drag-chute system and upgrades of the orbiters' tyres,
brakes, and nose-wheel steering mechanism. A crew escape system that would
allow astronauts to parachute from the orbiter under certain conditions
was also added. Finally, a new, streamlined management team was also put
in place that included experienced astronauts.
NASA
selected the orbiter Discovery for the “return to space” mission,
designated STS-26. On September 29, 1988, it blasted off from Kennedy
Space Centre, carrying a new Tracking and Data Relay Satellite identical
to the one that had been destroyed two and a half years before. The
Shuttle had returned to the skies, a much safer program. And never again
would any Shuttle launch be considered “routine.”
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