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STS-45

STS-45 was the 46th Space Shuttle mission and the 12th flight of the orbiter Atlantis, launched from Kennedy Space Center's Pad 39A on March 24, 1992, at 8:13 a.m. EST, after a one-day delay due to a hydrogen leak, carrying the Atmospheric Laboratory for Applications and Science-1 (ATLAS-1), a Spacelab mission dedicated to studying Earth's atmosphere, solar radiation, space plasma physics, and ultraviolet astronomy using 12 international instruments mounted on pallets in the cargo bay. The mission, commanded by Charles F. Bolden Jr. with pilot Brian Duffy and mission specialists Kathryn D. Sullivan, David C. Leestma, and C. Michael Foale, along with payload specialists Byron K. Lichtenberg and Dirk D. Frimout from Belgium, lasted 8 days, 22 hours, 9 minutes, and 28 seconds, completing 143 orbits at an altitude of 160 nautical miles with a 57-degree inclination before landing at Kennedy Space Center on April 2, 1992, at 6:23 a.m. EST, having traveled approximately 3.2 million miles. As the inaugural flight of the ATLAS series, STS-45 focused on gathering data to improve understanding of atmospheric chemistry and its interactions with solar activity, successfully performing the planned operations despite minor technical issues, including the first far-ultraviolet image of the Cygnus Loop supernova remnant. The mission marked several milestones, such as the first dedicated Spacelab flight for NASA's atmospheric research program and the debut of international collaboration through the European Space Agency, highlighted by Frimout becoming the first Belgian citizen to travel to space. Crew members conducted 11 development test objectives and 15 detailed supplementary objectives, including experiments on middeck facilities for materials processing and life sciences, while ATLAS-1 instruments like the Solar Spectrum Measurement instrument and the Far Ultraviolet Space Telescope provided critical data for climate and ozone layer studies. The STS-45 crew's diverse expertise enabled successful operations of the non-deployable payload, with , the first American woman to perform a spacewalk on a prior mission, contributing to payload activation, and Bolden later becoming Administrator. This flight underscored the program's role in international scientific partnerships and advanced , paving the way for subsequent ATLAS missions in 1993 and 1994.

Mission Background

Overview

STS-45 was the 46th flight of the Space Shuttle program and the 11th flight for the orbiter Atlantis. The mission launched on March 24, 1992, at 8:13:39 a.m. EST from Launch Complex 39A at NASA's Kennedy Space Center in Florida. Atlantis landed on April 2, 1992, at 6:23:06 a.m. EST on Runway 33 of the Shuttle Landing Facility at the same site. The mission lasted 8 days, 22 hours, 9 minutes, and 27 seconds, completing 143 orbits of while traveling a total distance of 5,211,340 kilometers. It operated in with a perigee of 282 kilometers, an apogee of 294 kilometers, and an inclination of 57 degrees. STS-45 carried a launch of 105,982 kilograms and landed with a of 93,009 kilograms. The primary objective was to conduct atmospheric and solar research using the non-deployable ATLAS-1 payload, consisting of pallets mounted in the orbiter's cargo bay as part of an international collaboration involving instruments from multiple countries.

Historical Context

STS-45 marked a pivotal moment in , serving as the inaugural dedicated mission for the Atmospheric Laboratory for Applications and Science (ATLAS-1), the first in a series of planned ATLAS flights aimed at studying Earth's atmosphere, solar influences, and related phenomena over an 11-year . Launched aboard , this mission followed the military-oriented STS-44 in November 1991 and preceded the servicing mission in May 1992, underscoring a programmatic emphasis on science-driven objectives in the post- era. After the 1986 disaster, reoriented its shuttle flights toward safer, more focused scientific endeavors, incorporating enhanced safety protocols such as stricter limits on and hydrogen concentrations in the launch configuration to mitigate risks identified in prior investigations. This shift highlighted a broader commitment to long-term environmental and solar research, building on the legacy of earlier missions like STS-40's United States Microgravity Laboratory-1 (USML-1) in June 1991, which had prioritized life sciences but paved the way for more specialized pallet-based configurations in ATLAS-1 to target atmospheric and solar interactions. The mission exemplified growing international collaboration in space science, involving alongside the (ESA) and contributions from agencies in , , , , the , and , with 12 instruments mounted on pallets in Atlantis's cargo bay. A notable milestone was the inclusion of as a , the first Belgian astronaut to fly in space, representing ESA and underscoring Belgium's entry into through this multinational effort. This cooperative framework evolved from the joint NASA-ESA initiatives of the 1980s, transitioning to targeted atmospheric-solar studies that integrated diverse instrumentation for comprehensive data collection on Earth's middle atmosphere and solar radiation effects. Pre-mission preparations encountered a one-day launch delay from March 23 to March 24, 1992, due to elevated concentrations of (860 ppm) and (750 ppm) in the orbiter's aft compartment, which exceeded allowable limits and required venting and to ensure . Once in orbit, the mission—originally planned for eight days—was extended by one day on flight day six, enabled by efficient use of cryogenic consumables, to gather additional scientific data on atmospheric processes and solar observations. This extension reinforced STS-45's role in advancing 's Mission to Planet Earth initiative, providing foundational datasets for subsequent ATLAS flights.

Crew

Members and Assignments

The STS-45 mission featured a crew of seven astronauts, comprising personnel and international partners, tasked with operating the Atmospheric Laboratory for Applications and Science-1 (ATLAS-1) payload. The commander was Charles F. Bolden Jr., on his third spaceflight, having previously flown on in 1986 and in 1990. The pilot was Brian Duffy, making his first spaceflight. Mission specialists included , the payload commander on her third flight (following in 1984 and in 1990); David C. Leestma, on his third flight (after and in 1989); and C. Michael Foale, on his maiden voyage. Payload specialists were Dirk D. Frimout from the (), on his first and only spaceflight, and Byron K. Lichtenberg, on his second flight (having flown on in 1983). Originally, American physicist Michael Lampton was selected as a but was replaced by Frimout due to medical reasons. Crew seating assignments followed standard Space Shuttle configuration, with positions numbered 1 through 7 for launch and adjusted slightly for landing if needed. The assignments were as follows (launch configuration):
SeatPositionAstronautRole
1CommanderCharles F. Bolden Jr.CDR (3rd flight)
2PilotBrian DuffyPLT (1st flight)
3Mission Specialist 1MS1 (3rd flight)
4Mission Specialist 2David C. LeestmaMS2 (3rd flight)
5Mission Specialist 3C. Michael FoaleMS3 (1st flight)
6Payload Specialist 1Dirk D. FrimoutPS1 (1st flight, ESA)
7Payload Specialist 2Byron K. LichtenbergPS2 (2nd flight)
To ensure continuous monitoring of the ATLAS-1 experiments over the mission's nine days, the crew was divided into two shifts: the Blue Team, consisting of Bolden, Duffy, , and Frimout; and the , comprising Leestma, Foale, and . This structure allowed for 24-hour operations, with teams alternating duties to oversee instrument activation, data collection, and payload adjustments. Among the crew, STS-45 marked first flights for Duffy, Foale, and Frimout, the latter becoming the first Belgian citizen to reach as an ESA representative. These milestones highlighted the 's role in expanding international participation in NASA-led operations.

Training and Responsibilities

The of STS-45 participated in an extensive pre-mission training regimen designed to prepare them for the complex operations of the Atmospheric Laboratory for Applications and Science-1 (ATLAS-1) payload and . This preparation included simulations of procedures, hands-on operation of scientific instruments, and drills for emergency scenarios such as system failures or medical contingencies, conducted primarily at 's in , . Additional training occurred at specialized facilities, including zero-gravity simulations aboard the KC-135 aircraft to replicate microgravity conditions for payload handling and experiment setup. The program emphasized the interdisciplinary demands of the , integrating expertise in vehicle control with scientific knowledge in , , and space plasma studies to ensure seamless execution of ATLAS-1 objectives. A key focus of the training was adapting to protocols, enabling 24-hour monitoring of experiments to capture time-sensitive data across orbital day and night cycles. members practiced alternating 12-hour shifts between the Blue Team—comprising Commander Charles F. Bolden Jr., Pilot Brian Duffy, Payload Commander , and Dirk D. Frimout—and the Red Team, which included Mission Specialists David C. Leestma and C. , along with Byron K. Lichtenberg. This structure promoted continuous science coverage, with in atmospheric and techniques allowing team members to serve as backups for specific instrument tasks, such as data calibration and real-time analysis. During the mission, responsibilities were clearly delineated to balance vehicle management and scientific operations. Bolden, as commander, oversaw all aspects of flight safety, navigation, and decision-making, while Duffy managed piloting tasks including ascent, orbital maneuvers, and re-entry preparations. The mission specialists—Sullivan, Leestma, and Foale—handled payload integration, shuttle systems monitoring, and contingency preparations, including readiness for extravehicular activities (EVAs), though none were required. Sullivan, serving as payload commander, coordinated overall ATLAS-1 activities, ensuring alignment between flight operations and experiment timelines. Payload Specialists Frimout, representing the (ESA), and Lichtenberg led the activation, calibration, and data monitoring of the 12 ATLAS-1 instruments, focusing on their expertise in solar radiation and to facilitate real-time adjustments during orbits. The inclusion of payload specialists underscored the 's collaborative nature, with Frimout's ESA background enhancing contributions to shared atmospheric research goals. This team dynamic, honed through coordinated training, exemplified the interdisciplinary approach needed for uninterrupted operations, fostering effective handovers between shifts to maximize scientific productivity.

Preparation and Launch

Vehicle Configuration

The , designated as Orbiter Vehicle OV-104, served as the primary spacecraft for STS-45, paired with External Tank ET-44 (Lightweight Tank LWT-37) and Solid Rocket Boosters BI-049 equipped with Redesigned Solid Rocket Motors (RSRM 360L021A for the left and 360W021B for the right). This configuration supported the mission's launch mass of approximately 4,495,720 pounds (2,039,000 kg), with the orbiter weighing 233,652 pounds (105,982 kg) at liftoff. The payload bay was adapted with two non-deployable Spacelab pallets to accommodate the ATLAS-1 instrument suite, comprising 12 scientific instruments from international partners including the United States, France, Germany, Belgium, Switzerland, the Netherlands, and Japan. The total payload mass, including ATLAS-1, the separate Shuttle Solar Backscatter Ultraviolet (SSBUV) instrument, and additional experiments, reached 20,371 pounds (9,237 kg). Integration involved mission-specific kits for secure mounting and power distribution, ensuring compatibility with the orbiter's systems without requiring structural alterations to the bay. Key supporting systems included the powerplant, which delivered 3,378 kilowatt-hours over the to support prolonged instrument operations, and the thermal control subsystem, which maintained nominal temperatures across the payload bay during door-open periods for observations. relay was handled via the orbiter's standard S-band and Ku-band antennas, interfacing with the Tracking and Data Relay Satellite System (TDRSS) for real-time transmission of scientific to ground stations. In the mid-deck area, six experiments were housed in lockers, including one Get Away Special (GAS) payload sponsored by the GAS program, along with investigations such as the Investigations into Polymer Membrane Processing (IPMP) and Space Tissue Loss (STL-01). The (RMS), or , was installed and operational but not utilized for any payload deployment or retrieval during the mission, serving as a contingency tool. Safety protocols incorporated the Shuttle Range Safety System, which functioned nominally throughout ascent and orbital phases.

Pre-Launch Activities

The Space Shuttle Atlantis, configured for STS-45, was rolled out to Launch Complex 39A at NASA's Kennedy Space Center on February 19, 1992, following integration of the ATLAS-1 payload in the orbiter's cargo bay during processing in the Vehicle Assembly Building. The payload, consisting of 12 international instruments mounted on Spacelab pallets, underwent final assembly and verification at Kennedy Space Center to ensure operational readiness for atmospheric and solar studies. Pre-launch preparations included loading and into the external tank, with extensive checks on propulsion systems and payload bay integrity. On March 23, 1992, the first launch attempt was scrubbed during tanking operations due to higher-than-allowable concentrations of hydrogen in the (peaking at 850 parts per million) and in the in the orbiter's aft engine compartment, resolved the following day through natural venting and additional monitoring with no leaks detected. The countdown for the March 24 launch proceeded smoothly after a 13-minute hold for low clouds over the emergency landing runway, with liftoff occurring at 8:13:40 a.m. under clear weather conditions and no further holds. The seven-member crew was inserted into the orbiter approximately two hours prior to launch, following standard suiting and transport procedures. Ground operations involved a coordinated effort by hundreds of NASA engineers, technicians, and contractors at , including final verification of ATLAS-1 instrument functionality through integrated systems tests to confirm alignment and calibration before tanking.

Orbital Mission

Timeline and Operations

Following launch on March 24, 1992, the achieved preliminary approximately 8.5 minutes after liftoff, marking the transition to the orbital phase of the STS-45 . Shortly after achieving on March 24, 1992, the activated the ATLAS-1 , initiating the primary scientific operations in the orbiter's payload bay. The encompassed 143 orbits over more than eight days, with the crew conducting daily operations that included opening the payload bay doors to enable unobstructed observations and . Continuous monitoring of and atmospheric phenomena occurred throughout the flight, supported by the ATLAS-1 positioned for exposure to space. On March 29, 1992, approved a one-day extension to the , allowing additional runtime for the instruments and ultimately achieving 95 percent of the planned objectives. Routine activities structured the crew's schedule, with shifts divided between red and blue teams to manage sleep, meals, and vehicle maintenance while ensuring uninterrupted oversight. Ground communications via the S-band facilitated real-time adjustments and data downlink to control.

In-Flight Events

During the STS-45 mission, the Space Experiments with Particle Accelerators (SEPAC) conducted beam emissions on its second and third firings, successfully generating artificial auroral-like phenomena in the upper atmosphere, which were observed and imaged by the Atmospheric Emissions Photometric Imaging (AEPI) instrument. A subsequent fuse failure in the SEPAC assembly halted further emissions, but the experiment met its primary objectives of studying beam-plasma interactions and auroral signatures. No major instrument failures occurred, though the Shuttle Solar Backscatter Ultraviolet (SSBUV) required adjustments for precise wavelength calibration. The Grille Spectrometer operated nominally but captured limited data on certain atmospheric profiles due to the moderate solar activity levels in March 1992, characterized by no major flares or storms. Crew members utilized the Remote Manipulator System () to maneuver and photograph the payload bay, capturing detailed views of the ATLAS-1 instruments for the first time during flight operations. Four licensed operators among the crew, including ESA payload specialist , conducted international communications via the Shuttle Amateur Radio Experiment (SAREX), linking with , ham operators, and ESA representatives to share mission insights. No extravehicular activities (EVAs) were planned or performed, as the mission focused on pallet-mounted experiments. Health monitoring proceeded routinely, with the crew participating in medical checks such as the Radiation Monitoring Equipment-III (RME-III) for dose assessment and the Visual Function Tester-II (VFT-II) for ocular evaluations, all reporting nominal physiological conditions despite fatigue from 24-hour shift schedules.

Payload and Experiments

ATLAS-1 Instruments

The ATLAS-1 payload on STS-45 consisted of 12 primary instruments mounted on two pallets in the shuttle's payload bay, designed to investigate interactions between , Earth's atmosphere, and through 14 coordinated experiments. These instruments focused on atmospheric composition, , and upper atmospheric phenomena, with contributions from the , , , , , , and .
InstrumentAcronymTechnical Purpose
Atmospheric Trace Molecule ATMOSInfrared absorption measurements of trace gases such as CO₂ and in the atmosphere from 10 to 150 km altitude.
Grille SpectrometerGRILLEInfrared emission and absorption analysis of middle and upper atmosphere chemistry from 15 to 150 km.
Millimeter Wave Atmospheric SounderMASMillimeter-wave emission profiling of (H₂O), (O₃), (CO), chlorine monoxide (ClO), temperature, and pressure from 10 to 100 km.
Solar Spectrum MeasurementSOLSPECSpectral analysis of from 200 to 2400 nm, including abundance determinations.
Solar Ultraviolet Spectral Irradiance MonitorSUSIMMonitoring of solar flux from 110 to 410 nm for profile studies.
Active Cavity Radiometer Irradiance Monitor IIACRIM-IIPrecise measurement of total to track variations.
Solar Constant MeasurementSOLCONHigh-precision absolute measurements of for and applications.
Atmospheric EmissionsALAE emission observations of thermospheric (H) and (D) concentrations.
Imaging Spectrometric ObservatoryISOLow-light spectrometric observations from 30 to 1300 nm on day and night sides of the .
Atmospheric Emissions Photometric ImagerAEPIImaging of upper atmosphere optical emissions from 200 to 750 nm to study auroral and phenomena.
Space Experiments with Particle AcceleratorsSEPACGeneration of artificial auroras using beams to investigate ionospheric and interactions.
Far Space TelescopeFAUSTFar- imaging from 1400 to 1800 Å of astronomical and atmospheric sources.
(Note: Mission documentation confirms 12 distinct instruments conducting 14 experiments.) Operationally, the instruments were configured for sun-pointing modes during observations to capture data and Earth-limb viewing for atmospheric , with the maintaining specific attitudes synchronized to orbital sunrise and sunset every 90 minutes. SEPAC involved active particle acceleration sequences. Calibration procedures included pre-flight ground tests at facilities like NASA's to verify instrument alignment and , followed by in-orbit adjustments on day 1 to account for variability and shuttle-induced perturbations. For instance, SUSIM used onboard lamps and comparison with data for real-time fine-tuning, ensuring accuracy across the 's 8 days.

Other Payloads

In addition to the primary ATLAS-1 payload, STS-45 carried several secondary experiments and systems in the and mid-deck, providing opportunities for student, commercial, and auxiliary research in microgravity. These payloads, totaling approximately 500 kg, were crew-managed without dedicated operational shifts and activated primarily during periods when ATLAS-1 observations were not nominal, ensuring efficient use of mission time. The Get Away Special (GAS) program enabled small-scale experiments, with one dedicated canister (G-229) focused on of semiconductors. This self-contained unit, a reflight from with improved monitoring, grew approximately 1 inch in diameter and 3.5 inches long over 11 hours, studying microgravity effects on material quality for potential electronics applications. Additionally, the (SSBUV-A) instrument, housed in two GAS canisters in the payload bay, performed calibration of ozone-measuring satellites by comparing shuttle-based UV data with instruments on NOAA and Nimbus-7 ; this was its fourth flight and first post-Mount Pinatubo eruption, capturing data on volcanic impacts. Mid-deck experiments emphasized biological, physiological, and environmental studies, all conducted in the crew compartment for accessibility. Key examples included:
  • Space Tissue Loss (STL): Examined microgravity-induced changes in muscle, bone, and endothelial cell growth using biological samples in a mid-deck locker, aiming to understand tissue degradation mechanisms.
  • Visual Function Tester-II (VFT-II): Assessed alterations in crew visual parameters through pre-, in-, and post-flight testing, providing data on microgravity's effects on eye function.
  • Radiation Monitoring Equipment-III (RME-III): A commercial payload that measured ionizing radiation exposure (gamma, electrons, neutrons, protons) in real-time, storing tissue-equivalent dose data for radiation protection analysis.
  • Shuttle Amateur Radio Experiment-II (SAREX-II): Facilitated amateur radio communications between the crew and ground stations, promoting educational outreach.
  • Cloud Logic to Optimize Use of Defense Systems (CLOUDS-1A): Investigated cloud cover variations and optical properties using a Nikon camera from multiple viewing angles to improve defense system modeling.
  • Investigations into Polymer Membrane Processing (IPMP): Explored microgravity influences on polymer membrane formation, focusing on the precipitation phase for filtration technology development.
Auxiliary systems supported overall data collection, including the Development Flight Instrumentation (DFI), which recorded orbiter performance metrics such as structural loads and thermal responses to validate vehicle engineering without reported anomalies. These secondary payloads collectively advanced understanding of microgravity environments while complementing the 's primary objectives.

Scientific Achievements

Key Results

The STS-45 mission, through the ATLAS-1 payload, yielded significant atmospheric discoveries, particularly in distributions. The Atmospheric (ATMOS) instrument detected concentrations in the above 50 km altitude, extending observations to higher levels than prior measurements and providing new insights into upper . Complementing this, the Millimeter-Wave Atmospheric Sounder (MAS) contributed to -related profiling through combined measurements of H₂O + 2CH₄ and correlations with ClO, while the Shuttle Solar Backscatter (SSBUV) and Solar Spectral Irradiance Monitor (SUSIM) instruments refined vertical profiles in the and lower by calibrating measurements against satellite data, enhancing accuracy in assessments. Solar observations from the mission confirmed subtle variations in the Sun's total energy output, vital for understanding influences. The Active Cavity Radiometer Irradiance Monitor II (ACRIM-II) and (SOLCON) instruments measured daily fluctuations in the of approximately 0.1%, with precision to 0.1%, validating models of activity impacts on ; SOLCON reported a value of 1361.5 ± 2.3 W/m². Additionally, the Solar Spectrum (SOLSPEC) instrument established baseline measurements of and visible , which served as references for global abundance estimates and atmospheric studies. In auroral and ultraviolet research, the mission achieved breakthroughs in plasma interactions and astronomical imaging. The Space Experiment with Particle Accelerators (SEPAC) and Atmospheric Emissions Photometric Imaging (AEPI) experiments successfully generated and imaged artificial auroras using electron beam injections into the ionosphere, revealing details on auroral morphology, double layers, and radio emissions like whistlers. Meanwhile, the Far Ultraviolet Space Telescope (FAUST) performed a comprehensive far-ultraviolet sky survey in the 1400-1800 Å range, capturing high-resolution images of the Cygnus Loop supernova remnant and other diffuse sources, despite a minor power issue. Overall, STS-45 met 95% of its scientific objectives across 14 experiments, generating extensive datasets that supported long-term modeling of atmospheric dynamics and -terrestrial interactions.

Data Analysis and Impact

Post-mission data from STS-45's ATLAS-1 payload was downlinked via telemetry to NASA's and other ground facilities for initial processing and archiving. Calibration procedures involved cross-verification against pre-flight ground-based instruments and in-situ validations, such as self-calibrating occultation measurements from the instrument compared to photochemical models for like and nitrogen oxides. For example, methane-related measurements from the Millimeter-wave Atmospheric Sounder () were validated through comparisons with concurrent balloon-borne observations, ensuring accuracy in stratospheric profiles. These efforts culminated in peer-reviewed publications between 1993 and 1995, including analyses of spectral irradiance by the SOLSPEC instrument, as detailed in Thuillier et al. (1998), which provided high-precision UV data calibrated against ground references. The processed ATLAS-1 datasets proved foundational for advancing studies, offering baseline measurements of stratospheric trace gases that highlighted chlorine-driven losses during the declining phase of 22. They also contributed to solar-terrestrial interaction models by quantifying variations and their atmospheric effects, enabling better predictions of middle atmosphere dynamics. These insights directly influenced the design and execution of subsequent ATLAS-2 (STS-56, 1993) and ATLAS-3 (STS-66, 1994) missions, which built on STS-45's validation techniques to extend observations across the . On a broader scale, ATLAS-1 fostered cooperation through ESA's involvement, including from the GRILLE spectrometer and Belgian contributions, which integrated European atmospheric models with datasets. The mission advanced techniques via SOLSPEC's absolute irradiance measurements, establishing standards for space-based solar monitoring that reduced uncertainties in calculations. While the core findings remain robust, recent assessments suggest reanalysis of the datasets using modern models to account for updated forcings and refine long-term trend attributions. ATLAS-1 datasets are preserved in NASA's Planetary Data System and Goddard Earth Sciences Data and Information Services Center archives, facilitating ongoing research. In the 2020s, these data have supported solar cycle predictions, particularly for Cycle 25, by providing historical irradiance benchmarks integrated into heliospheric models for space weather forecasting.

Landing and Post-Mission

Reentry and Landing

The deorbit burn for STS-45 was initiated at 10:20:55 GMT on April 2, 1992 (mission elapsed time of 8 days, 21 hours, 7 minutes, 16 seconds), using both Orbital Maneuvering System engines for a duration of 220.6 seconds, resulting in a velocity reduction of 408.3 feet per second (approximately 124 m/s) to set up the reentry trajectory. This maneuver targeted a reentry interface at 400,000 feet altitude, with the orbiter Atlantis entering Earth's atmosphere at a velocity of about 25,000 feet per second (Mach 25). The mission had been extended by one day to maximize science operations, allowing additional time for payload activities before deorbit. During reentry, Atlantis followed a standard lifting body profile, experiencing peak heating within thermal protection system limits and peak deceleration forces of approximately 1.5 , with aerodynamic performance nominal throughout. Atmospheric conditions at the were nominal, with clear weather supporting the primary landing site. Touchdown occurred on Runway 33 at 6:23:06 a.m. EST (11:23:06 GMT), during the 143rd , with main gear followed by nose gear deployment 8 seconds later and rollout distance of 9,227 feet over 60 seconds. The landing weight was 205,042 pounds, and braking was initiated at 135.3 knots with no anomalies in tire pressures or brake performance (energies 25.9–29.32 million foot-pounds). Post-landing, the crew egressed safely approximately 40 minutes after wheels stop, and orbiter safing procedures were completed, including shutdown by 11:38:10 GMT, with all systems secured nominally.

Mission Evaluation

The STS-45 mission achieved 95 percent of its scientific objectives, with all primary goals met and the majority of secondary objectives and detailed test objectives (DTOs) and supplementary objectives (DSOs) successfully completed, demonstrating the effectiveness of the ATLAS-1 payload configuration for atmospheric and solar research. Minor issues, including a one-day launch delay due to and propellant leaks exceeding limits during pre-launch checks, were resolved through enhanced cryogenic system troubleshooting without compromising mission timelines or . Instrument glitches, such as erratic performance in 1's gas generator heater and Ku-band antenna frequency shifts affecting data transmission, were mitigated in flight and did not impact overall payload operations. Anomalies during STS-45 were limited and posed no risks to the or vehicle. The launch on March 23, 1992, stemmed from the concentration exceedances, but subsequent repairs ensured a nominal ascent on March 24. No significant in-flight interference affected the Grille Spectrometer or other ATLAS-1 instruments, though minor thermal protection system () impacts from debris—totaling 122 sites, 18 larger than one inch—were noted post-landing and assessed as non-critical. Ku-band communication disruptions, lasting up to 30 minutes on several passes, were traced to tracking errors but resolved via ground adjustments, maintaining data integrity. Key lessons from STS-45 informed future operations, particularly in efficiency and support. The mission's extension to nine days highlighted the value of flexible shift scheduling, allowing additional without fatigue issues and optimizing 24-hour monitoring. Enhanced data downlink procedures were recommended to address Ku-band vulnerabilities, emphasizing redundant tracking for uninterrupted transmission in subsequent ATLAS missions. Overall, the flight validated improvements in external tank-orbiter interface sealing to prevent debris, reducing risks for follow-on flights. Original mission records focused primarily on immediate operational outcomes, somewhat underemphasizing the long-term impacts of ATLAS-1 datasets on atmospheric modeling; modern reanalyses, including those integrating STS-45 observations with data from the 2000s onward, have since clarified these contributions to studies. As of , no major archival updates or revisions to the 's evaluation are required, with its scientific legacy enduring through ongoing applications in . The 's success in achieving key atmospheric and measurements underscored the program's role in multidisciplinary .

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