1 February 2003, 09:00:18 a.m., Eastern Standard Time: Space Shuttle Columbia, nearing the end of Mission STS-107, traveling Mach 19.5 (13,434 miles per hour, 21,620 kilometers per hour) at 209,800 feet (63,950 meters) over Texas, suffered catastrophic structural failure and disintegrated. All seven members of the crew were killed.
81.7 seconds after liftoff on 16 January, Columbia was at approximately 66,000 feet (20,100 meters) altitude and 12.5 miles (20.1 kilometers) down range, accelerating through Mach 2.46 (1,623 miles per hour, 2,612 kilometers per hour). Several pieces of insulating foam broke off of the external fuel tank (what NASA referred to as “foam shedding”) and struck the leading edge and underside of Columbia‘s left wing. It is believed that at least one of these pieces of foam punctured a hole in the wing’s surface, estimated to be 6 inches × 10 inches (15 × 25 centimeters).
Columbia was scanned as it passed overhead the Starfire Optical Range at Kirtland Air Force Base, New Mexico, at approximately 7:57 a.m., CST, (13:57 UTC) 1 February 2003. Debris can be seen coming from the shuttle’s left wing. (NASA Johnson Space Flight Center)
During reentry, the internal structure of the wing was no longer protected by the heat resistant material of the leading edge. The extreme heat caused structural failure.
Space Shuttle Columbia (OV-102) launches on Mission STS-107, 16 January 2003. (NASA)
Columbia (OV-102) was America’s first space shuttle. It flew into space for the first time 11 April 1981. STS-107 was its 28th flight. During those missions, Columbia orbited the Earth 4,808 times and spent 300 days, 17 hours, 40 minutes, 22 seconds in space flight. 160 astronauts served aboard her. She traveled 125,204,911 miles (201,497,722 kilometers).
The Space Shuttle Columbia disintegrated over North America during reentry, 1 February 2003. (AP)
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Space Shuttle Columbia STS-107 flight crew. Front row, left to right: Colonel Rick Douglas Husband, U.S. Air Force, Mission Commander; Kalpana Chawla, Ph.D., Mission Specialist; Commander William Cameron McCool, U.S. Navy, Pilot. Back row, left to right: Captain David McDowell Brown, M.D., U.S. Navy, Mission Specialist; Captain Laurel Blair Salton Clark, M.D., U.S. Navy, Mission Specialist; Lieutenant Colonel Michael Phillip Anderson, U.S. Air Force, Mission Specialist; Colonel Ilan Ramon, Israeli Air Force, Payload Specialist. (NASA)
The flight crew of Apollo 14, Edgar D. Mitchell, Alan B. Shepard and Stuart A. Roosa, stand in front of their Saturn V rocket, AS-509, at Space Flight Complex 39A, Kennedy Space Center. (NASA)
31 January 1971, 04:03:02 a.m., Eastern Standard Time: Apollo 14 (AS-509) lifted off for The Moon from Space Flight Launch Complex 39A, Kennedy Space Center, Cape Canaveral, Florida. The Mission Commander was Captain Alan Bartlett Shepard, Jr., United States Navy. The Command Module Pilot was Colonel Stuart Allen Roosa, United States Air Force, and the Lunar Module Pilot was Captain Edgar Dean Mitchell, Sc.D., United States Navy. Their destination was the Fra Mauro Highlands.
Apollo 14 was the eighth manned mission of the Apollo Program, and the third to land on the surface of the moon.
Alan Shepard was the first American astronaut. He flew into space aboard a Mercury spacecraft, Freedom 7, launched from Cape Canaveral by a Redstone rocket, 5 May 1961.
Captain Alan B. Shepard, Jr., Mission Commander, Apollo 14. (NASA)
Mitchell and Roosa had not flown in space before. This would be their only space flight.
The Apollo Command/Service Module was built by the Space and Information Systems Division of North American Aviation, Inc., at Downey, California.
The SPS engine was an AJ10-137, built by Aerojet General Corporation of Azusa, California. It burned a hypergolic fuel combination of Aerozine 50 and nitrogen tetraoxide, producing 20,500 pounds of thrust (91.19 kilonewtons). It was designed for a 750 second burn, or 50 restarts during a flight.
The Saturn V rocket was a three-stage, liquid-fueled heavy launch vehicle. Fully assembled with the Apollo Command and Service Module, it stood 363 feet (110.642 meters) tall. The first and second stages were 33 feet (10.058 meters) in diameter. Fully loaded and fueled the rocket weighed 6,200,000 pounds (2,948,350 kilograms). It could lift a payload of 260,000 pounds (117,934 kilograms) to Low Earth Orbit.
The first stage was designated S-IC. It was designed to lift the entire rocket to an altitude of 220,000 feet (67,056 meters) and accelerate to a speed of more than 5,100 miles per hour (8,280 kilometers per hour). The S-IC stage was built by Boeing at the Michoud Assembly Facility, New Orleans, Louisiana. It was 138 feet (42.062 meters) tall and had an empty weight of 290,000 pounds (131,542 kilograms). Fully fueled with 203,400 gallons (770,000 liters) of RP-1 and 318,065 gallons (1,204,000 liters) of liquid oxygen, the stage weighed 5,100,000 pounds (2,131,322 kilograms). It was propelled by five Rocketdyne F-1 engines, producing 1,522,000 pounds of thrust (6770.19 kilonewtons), each, for a total of 7,610,000 pounds of thrust at Sea Level (33,850.97 kilonewtons). These engines were ignited seven seconds prior to lift off and the outer four burned for 168 seconds. The center engine was shut down after 142 seconds to reduce the rate of acceleration. The F-1 engines were built by the Rocketdyne Division of North American Aviation at Canoga Park, California.
The S-II second stage was built by North American Aviation at Seal Beach, California. It was 81 feet, 7 inches (24.87 meters) tall and had the same diameter as the first stage. The second stage weighed 80,000 pounds (36,000 kilograms) empty and 1,060,000 pounds loaded. The propellant for the S-II was liquid hydrogen and liquid oxygen. The stage was powered by five Rocketdyne J-2 engines, also built at Canoga Park. Each engine produced 232,250 pounds of thrust (1,022.01 kilonewtons), and combined, 1,161,250 pounds of thrust (717.28 kilonewtons).
Stuart A. Roosa wearing an ILC Dover A7L full-pressure suit, 31 January 1971. (NASA)
The Saturn V third stage was designated S-IVB. It was built by Douglas Aircraft Company at Huntington Beach, California. The S-IVB was 58 feet, 7 inches (17.86 meters) tall with a diameter of 21 feet, 8 inches (6.604 meters). It had a dry weight of 23,000 pounds (10,000 kilograms) and fully fueled weighed 262,000 pounds. The third stage had one J-2 engine and also used liquid hydrogen and liquid oxygen for propellant. The S-IVB would place the Command and Service Module into Low Earth Orbit, then, when all was ready, the J-2 would be restarted for the Trans Lunar Injection.
Apollo 14’s S-IVB third stage, after the Lunar Module Antares was extracted. The S-IVB was then directed to impact the Moon, 4 February 1971. (NASA)
Eighteen Saturn V rockets were built. They were the most powerful machines ever built by man.
Apollo 14 lifts off from Launch Complex 39A, Kennedy Space Center, 4:03:02 a.m., EST, 31 January 1971. (NASA)
Space Shuttle Challenger (STS-51L) was launched from Launch Complex 39B, Kennedy Space Center, at 16:38 UTC, 28 January 1986. (Thom Baur/AP)
28 January 1986, 11:38:00 a.m. (EST): The Space Shuttle Challenger (OV-99) lifted off from Launch Complex 39B at the Kennedy Space Center, Cape Canaveral, Florida, on Mission STS-51L.
At liftoff, an O-ring seal between segments of the right Solid Rocket Booster (SRB) began leaking. Superheated gases breached the seal and began to burn laterally.
“At 58.778 seconds into powered flight, a large flame plume is visible just above the SRB exhaust nozzle indicating a breach in the motor casing.” (NASA)
The venting rocket exhaust burned through the SRB attachment strut and into the liquid hydrogen tank in the lower section of the External Tank. The aft portion of the liquid hydrogen tank failed and drove the tank vertically upward into the liquid oxygen tank. Both tanks ruptured and the propellants detonated.
1 minute, 13 seconds after liftoff, Challenger was accelerating through Mach 1.62 (1,069 miles per hour, 1,720 kilometers per hour) at approximately 46,000 feet (14,020 meters) when the explosion of the external tank caused the space shuttle to suddenly veer away from its flight path. The shuttle was subjected to aerodynamic forces far beyond its design limits and it was torn apart.
Challenger’s external tank, containing liquid hydrogen and liquid oxygen, exploded 1 minute 13 seconds after liftoff. The two solid rocket boosters flew off in different directions. (Bruce Weaver/AP)
The crew cabin, with its seven astronauts aboard, broke away from the disintegrating shuttle assembly and continued upward for another 25 seconds to approximately 65,000 feet (19,080 meters), then began a long fall to the ocean below.
2 minutes 45 seconds after the explosion, the cabin impacted the surface of the Atlantic Ocean at 207 miles per hour (333 kilometers per hour). The entire crew was killed.
The crew cabin of Space Shuttle Challenger is visible near the end of the smoke plume at the upper center of this photograph, still climbing at supersonic speed. (NASA)
I watched this terrible tragedy as it happened, live on television. I will never forget.
The explosion occurred 1 minute, 13 seconds after liftoff. (NASA)
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Space Shuttle Challenger STS-51L Flight Crew. Front Row, left to right, Captain Michael J. Smith, U.S. Navy; Lieutenant Colonel Francis R. Scobee, U.S. Air Force; Ronald Ervin McNair. Back Row, left to right: Lieutenant Colonel Ellison S. Onizuka, U.S. Air Force; Sharon Christa McAuliffe; Gregory Bruce Jarvis; Judith Arlene Resnick. (NASA)
The crew of Apollo 1. Left to right, Lieutenant Colonel Virgil I. Grissom, United States Air Force, Lieutenant Colonel Edward H. White II, United States Air Force, and Lieutenant Commander Roger B. Chaffee, United States Navy. (National Aeronautics and Space Administration)
27 January 1967: During a “plugs out” test of the Apollo 1 Command Module, two weeks ahead of the scheduled launch of the Apollo/Saturn 1B AS-204—the first manned Apollo Program space flight—a fire broke out in the pressurized pure oxygen environment of the capsule and rapidly involved the entire interior.
The pressure rapidly built to 29 pounds per square inch (200 kPa) and 17 seconds later, at 23:31:19.4 UTC, the capsule ruptured.
The three astronauts, Lieutenant Colonel Virgil I. Grissom, United States Air Force, Lieutenant Colonel Edward H. White II, United States Air Force, and Lieutenant Commander Roger B. Chaffee, United States Navy, were killed.
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NASA has a detailed summary of the accident and investigation at:
“The interior of a crater surrounding the Mars Exploration Rover Opportunity at Meridiani Planum on Mars can be seen in this color image from the rover’s panoramic camera. This is the darkest landing site ever visited by a spacecraft on Mars. The rim of the crater is approximately 10 meters (32 feet) from the rover. The crater is estimated to be 20 meters (65 feet) in diameter. Scientists are intrigued by the abundance of rock outcrops dispersed throughout the crater, as well as the crater’s soil, which appears to be a mixture of coarse gray grains and fine reddish grains. Data taken from the camera’s near-infrared, green and blue filters were combined to create this approximate true color picture, taken on the first day of Opportunity’s journey. The view is to the west-southwest of the rover.” (NASA Jet propulsion Laboratory)
25 January 2004: Mars Exploration Rover–B, named Opportunity, landed at Meridiani Planum on the surface of Mars at 5:05 a.m., UTC SCET (Spacecraft Event Time) and rolled into a small crater, approximately 22 meters (72 feet) in diameter.
Meridiani Planum is near the center of this image of Mars, photographed from the Mars Orbiter Mission, 28 September 2014, at an altitude of 74,582 kilometers (46,343 miles). (The Bruce Murray Space Image Library)
The crater would later be named Eagle Crater, and the landing site is named Challenger Memorial Station. The site is on the opposite side of the planet from Opportunity‘s twin, MER-A, Spirit.
“This image taken by the panoramic camera onboard the Mars Exploration Rover Opportunity shows the rover’s now-empty lander, the Challenger Memorial Station, at Meridiani Planum, Mars. The image was acquired on the 24th martian day, or sol, of Opportunity’s mission at approximately 13:00 Local Solar Time. This is a mosaic image consisting of 12 color images acquired with the camera’s red, green and blue filters. The color balance has been set to approximate the colors that a human eye would see.” (NASA/JPL/Cornell)Artist’s conception of a NASA Mars Exploration Rover on the surface of Mars. (JPL)
