Колумбия ғарыш кемесінің 1999 жылғы ұшырылысындағы ақаулар және қауіпсіздік шаралары

1999 American crewed spaceflight to deploy the Chandra X ray Observatory

SeatLaunchLandingSeats 1–4 are on the Flight Deck. Seats 5–7 are on the Middeck. S1CollinsCollinsS2AshbyAshbyS3TogniniColemanS4HawleyHawleyS5ColemanTognini

During the main engine ignition sequence, a gold pin used to plug an oxidizer post in the Space Shuttle's number three (right) engine came loose and was violently ejected, striking the engine nozzle's inner surface and tearing open three cooling tubes containing hydrogen. These ruptures resulted in a leak upstream of the main combustion chamber. This anomalous event and the automatic response to the leak by the right engine's controller did not violate any launch commit criteria and liftoff proceeded normally. However, approximately 5 seconds after liftoff, an electrical short disabled the center engine's primary digital control unit, DCU A, and the right engine's backup unit, DCU B. The center and right engines continued to operate on their remaining DCUs for the rest of powered flight to orbit. The redundant set of DCUs in each engine controller saved Columbia and her crew from potential catastrophe, as shutdown of two engines at that point in the flight would have resulted in a very risky contingency abort with no guarantee of success. The electrical short was later discovered to have been caused by poorly routed wiring, which had rubbed on an exposed screw head. This wiring issue led to a program wide inspection of the wiring in all orbiters. Because of the leak in the right engine, its controller sensed a decrease in power or thrust—measured indirectly as main combustion chamber pressure—since the leaking hydrogen was not being burned in the SSME's two pre burners or the main combustion chamber. To bring the engine back up to the commanded thrust level, the controller opened the oxidizer valves a bit more than normal. The hydrogen leak and increased oxidizer consumption resulted in the right engine deviating from the desired oxygen/hydrogen mixing ratio of 6.03 and running hotter than normal. The increased oxidizer consumption during ascent resulted in a premature shutdown of all three engines near the end of the projected burn due to low liquid oxygen level sensed in the External Tank. Though the premature shutdown resulted in a velocity lower than targeted, the vehicle safely achieved its intended orbit and completed the mission as planned. This incident brought on a maintenance practice change that required damaged oxidizer posts to be removed and replaced as opposed to being intentionally plugged, as was the practice beforehand. Three days previously, in the first launch attempt, the launch was stopped at T−7 seconds, just prior to the SSMEs' ignition sequence, due to a senior console operator manually triggering a cutoff in the countdown. It was later determined that the console operator, monitoring the hydrogen gas concentration in the Space Shuttle's aft compartment, where the three SSMEs are located, saw a hydrogen increase spike above the Launch Commit Criteria redline, for a single sample just prior to main engine start. Subsequent troubleshooting and analysis indicated the most likely cause was the mass spectrometer instrument experienced a data anomaly in the high vacuum region of the instrument for a single sample. The system performance was nominal prior to the cut off and during subsequent launch attempts.

The primary objective of the STS 93 mission was to deploy the Chandra X ray Observatory (formerly the Advanced X ray Astrophysics Facility) with its Inertial Upper Stage booster. At its launch, Chandra was the most sophisticated X ray observatory ever built. It is designed to observe X rays from high energy regions of the universe, such as hot gas in the remnants of exploded stars. Other payloads on STS 93 included the Midcourse Space Experiment (MSX), the Shuttle Ionospheric Modification with Pulsed Local Exhaust (SIMPLEX), the Southwest Ultraviolet Imaging System (SWUIS), the Gelation of Sols: Applied Microgravity Research (GOSAMR) experiment, the Space Tissue Loss – B (STL B) experiment, a Light mass Flexible Solar Array Hinge (LFSAH), the Cell Culture Module (CCM), the Shuttle Amateur Radio Experiment – II (SAREX – II), EarthKAM, Plant Growth Investigations in Microgravity (PGIM), the Commercial Generic Bioprocessing Apparatus (CGBA), the Micro Electrical Mechanical System (MEMS), and the Biological Research in Canisters (BRIC). The Shuttle Ionospheric Modification with Pulsed Local Exhaust (SIMPLEX) payload activity researched the source of Very High Frequency (VHF) radar echoes caused by the orbiter and its OMS engine firings. The Principal Investigator (PI) used the collected data to examine the effects of orbital kinetic energy on ionospheric irregularities and to understand the processes that take place with the venting of exhaust materials. The Southwest Ultraviolet Imaging system (SWUIS) was based around a Maksutov design ultraviolet (UV) telescope and a UV sensitive, image intensified charge coupled device (CCD) camera that frames at video frame rates. Scientists can obtain sensitive photometric measurements of astronomical targets. The objective Gelation of Sols: Applied Microgravity Research (GOSAMR) experiment was to investigate the influence of microgravity on the processing of gelled sols. In particular, the purpose was to demonstrate that composite ceramic precursors composed of large particulates and small colloidal sols can be produced in space with more structural uniformity. The focus of the Space Tissue Loss – B (STL B) experiment was direct video observation of cells in culture through the use of a video microscope imaging system with the objective of demonstrating near real time interactive operations to detect and induce cellular responses. The Light mass Flexible Solar Array Hinge (LFSAH) payload consisted of several hinges fabricated from shape memory alloys. Shape memory deployment hinges offered controlled shockless deployment of solar arrays and other spacecraft appendages. LFSAH demonstrated this deployment capability for a number of hinge configurations. The objectives of the Cell Culture Module (CCM) were to validate models for muscle, bone, and endothelial cell biochemical and functional loss induced by microgravity stress; to evaluate cytoskeleton, metabolism, membrane integrity and protease activity in target cells; and to test tissue loss medications. The Shuttle Amateur Radio Experiment (SAREX II) demonstrated the feasibility of amateur short wave radio contacts between the shuttle and ground based amateur radio operators. SAREX also served as an educational opportunity for schools around the world to learn about space by speaking directly to astronauts aboard the shuttle via amateur radio. The EarthKAM payload conducted Earth observations using the Electronic Still Camera (ESC) installed in the overhead starboard window of the Aft Flight Deck. The Plant Growth Investigations in Microgravity (PGIM) payload experiment used plants to monitor the space flight environment for stressful conditions that affect plant growth. Because plants cannot move away from stressful conditions, they have developed mechanisms that monitor their environment and direct effective physiological responses to harmful conditions. The Commercial Generic Bioprocessing Apparatus (CGBA) payload hardware allowed for sample processing and stowage functions. The Generic Bioprocessing Apparatus – Isothermal Containment Module (GBA ICM) was temperature controlled to maintain a preset temperature environment, controlled the activation and termination of the experiment samples, and provided an interface for crew interaction, control and data transfer. The Micro Electrical Mechanical System (MEMS) payload examined the performance, under launch, microgravity, and reentry conditions of a suite of MEMS devices. These devices included accelerometers, gyroscopes, and environmental and chemical sensors. The MEMS payload was self contained and required activation and deactivation only. The Biological Research in Canisters (BRIC) payload was designed to investigate the effects of space flight on small arthropod animals and plant specimens. The flight crew was available at regular intervals to monitor and control payload/experiment operations. Columbia landing at Kennedy Space Center marked the twelfth night landing in the Shuttle program's history. Five had been at Edwards Air Force Base in California and the rest KSC. To date, there had been 19 consecutive landings at KSC and 25 of the last 26 had been there.

In 2001, Coin World reported the revelation (via a FOIA document request) that the United States Mint had struck 39 examples of the 2000 Sacagawea dollar in gold in June 1999 at the West Point Mint. The planchets came from specially prepared ½ troy oz $25 American Gold Eagle Bullion Planchets. Why they were struck is not known; speculation is that this was an attempt by the mint to offer "Premium" collectibles in conjunction with the newly released Sacagawea dollar in 2000. Twenty seven were soon melted and the remaining 12 were on board Space Shuttle Columbia for the July 1999 STS 93 mission. Two examples then popped up at two separate events; one during a Private Congressional Dinner in August 1999, and another example at the Official First Strike ceremonies in November. The coins remained at Mint Headquarters under lock and key until they were transferred in 2001 to Fort Knox. The strikes are considered to be illegal due to the Coinage regulations in place. In 2007, the Mint announced it would for the first time publicly display the 12 space flown gold dollars at the American Numismatic Association's World's Fair of Money in Milwaukee, Wisconsin.