Space Shuttle Challenger Final Mission
The Space Shuttle program project originated back in the 1960s and was
inspired by the Apollo lunar landing. The objective of the space shuttle
was to provide frequent, economical transport to low earth space that
was accessible to the public. The Space Shuttle was designed to be the
equivalent of a “space ferry”. This ambitious idea of reusable
spacecraft had initially been presented to President Nixon in the early
1970’s, with a relatively low annual cost estimate of $4 to $6 billion.
The final project components consisted of an Earth-orbiting space
station and the Space Ferry Shuttle. It also led to the birth of the
National Space Transportation System.
The task of building a safe, durable, economic and reusable spacecraft
was both complex and challenging. It involved several National
Aeronautics and Space Administration (NASA) centers: operation,
development and maintenance facilities. The program employed prime
industrial contractors and subcontractors, involving the contributions
of several thousand individuals.
Space Shuttle Development was divided between several centers each responsible for a specific task.
Rockwell International Corporation’s Space Transportation Systems
division provided the design and development of the Space Shuttle
Orbiter;
Martin Marietta Denver Aerospace developed and constructed the External Tank;
Morton Thiokol Corporation designed and manufactured the Solid Rocket Boosters (SRB’s);
Rocketdyne, a division of Rockwell, developed the Orbiter and main engines.
Managerial obligations over the program development were allocated among three field centers:
Johnson Space Center (“Johnson”) in Houston, Texas oversaw the Orbiter
Marshall Space Flight Center (“Marshall”) in Huntsville, Alabama was
responsible for the Orbiter’s main engines, the External Tank and the
SRB’s;
Kennedy Space Center (“Kennedy”) in Merritt Island, Florida was tasked
with assembling and checking the Space Shuttle components, and
conducting launches.
The Space Shuttle development program experienced numerous challenges
including budgetary constraints, engineering complexities, and project
time-delivery limitations. The program eventually completed orbital
testing in 1981 and went into operation in mid-1982. Through January
1986, the NASA Space Shuttle flew 24 successful missions over a 57-month
period. The most frequent shuttlecraft used was Challenger,
accomplishing nine successful flights. It would not survive a tenth
attempt.
Challenger was the craft chosen for the launch of mission 51-L, which
was postponed three times. The third postponement occurred an evening
before the third planned launch date on January 25, 1986. That evening,
management held a conference call to review and discuss weather
conditions forecast for Kennedy. Due to unfavorable weather conditions,
the launch was re-scheduled to January 27th. The Challenger crew
started their day at 5:07 am to prepare for the launch. However, by 9 am
that morning, the launch had been halted yet again due to the problems
with an exterior hatch handle. By the time the issue was fixed, the
winds on the Kennedy launch pad had increased to an unacceptable level
and the mission was postponed again to the next day.
Later that evening, the temperature dropped to about twenty degrees
Fahrenheit. The Space Shuttle management team sent engineers to assess
the Orbiter for potential issues associated with the low temperatures
for the upcoming launch. No issues were identified and the launch was
permitted to proceed as planned. However, during the night, ice
accumulated in the launch area. After inspection the next morning, the
project manager decided to allow for additional time for the accumulated
ice to melt. A final assessment of the icy conditions was then
performed at 11:15 am, with the spacecraft finally cleared for launch.
The Flight 51-L crew then boarded the spacecraft. The Challenger flight
began at 11:38:00.010 am on January 28th, 1986. Challenger’s signal was
lost by Mission Control only 73 short seconds later…
The spacecraft flew in a cloud of fire just 73 seconds after liftoff at
an altitude of 46,000 feet. Further investigation showed that no
explosion had taken place. The fatal problem involved a seal in the
right Solid-fuel Rocket Booster. The Challenger crew did not die
immediately. The passenger cabin was found to have been torn away from
the shuttle, breaking apart and flying for a couple of seconds until
hitting the surface of the Atlantic Ocean at more than 200 mph.
This resulted in the highest profile catastrophe in the NASA Space Program.
We Select risk quantification enterprise risk management (ERM) processes. Please identify one cognitive biases on the slide