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This STS-68 patch was designed by artist Sean Collins. Exploration of Earth from space is the focus of the design of the insignia, the second flight of the Space Radar Laboratory (SRL-2). SRL-2 was part of NASA's Mission to Planet Earth (MTPE) project. The world's land masses and oceans dominate the center field, with the Space Shuttle Endeavour circling the globe. The SRL-2 letters span the width and breadth of planet Earth, symbolizing worldwide coverage of the two prime experiments of STS-68: The Shuttle Imaging Radar-C and X-Band Synthetic Aperture Radar (SIR-C/X-SAR) instruments; and the Measurement of Air Pollution from Satellites (MAPS) sensor. The red, blue, and black colors of the insignia represent the three operating wavelengths of SIR-C/X-SAR, and the gold band surrounding the globe symbolizes the atmospheric envelope examined by MAPS. The flags of international partners Germany and Italy are shown opposite Endeavour. The relationship of the Orbiter to Earth highlights the usefulness of human space flights in understanding Earth's environment, and the monitoring of its changing surface and atmosphere. In the words of the crew members, the soaring Orbiter also typifies the excellence of the NASA team in exploring our own world, using the tools which the Space Program developed to explore the other planets in the solar system.


Occurred 30 years ago

Second of the Space Radar Laboratory (SRL-2).



mission duration

11 days, 5 hours, 46 minutes


September 30, 1994


October 11, 1994
Six astronauts in orange spacesuits pose for crew photo with a BAKER WILCUTT SMITH AND WISOFF BURSCH JONES sign.
These six NASA astronauts composed the crew of the STS-68 mission that launched aboard the Space Shuttle Endeavour on September 30, 1994. Standing are, left to right, Michael A. Baker, mission commander; and Terrence W. Wilcutt, pilot. On the front row are, left to right, Thomas D. Jones, payload commander; and Peter J. K. (Jeff) Wisoff, Steven L. Smith, and Daniel W. Bursch, all mission specialists. STS-68 marked the second flight of the Space Radar Laboratory, part of NASA’s mission to planet Earth.

STS-68 Mission Facts

Mission: Space Radar Laboratory (SRL-2)
Space Shuttle: Endeavour
Launch Pad: 39A
Launched: September 30, 1994, 7:16:00 a.m. EDT
Landing Site: Edwards Air Force Base, Calif.
Landing: October 11, 1994, 10:02:08 a.m. PDT
Runway: 22
Rollout Distance: 8,495 feet
Rollout Time: 60 seconds
Revolution: 182
Mission Duration: 11 days, 5 hours, 46 minutes, 8 seconds
Orbit Altitude: 120 nautical miles
Orbit Inclination: 57 degrees
Miles Traveled: 4.7 million


Michael A. Baker, Commander
Terrence W. Wilcutt, Pilot
Thomas D. Jones, Payload Commander
Steven L. Smith, Mission Specialist
Daniel W. Bursch, Mission Specialist
Peter J. K. Wisoff, Mission Specialist

Mission Highlights

STS-68 marked second flight in 1994 of Space Radar Laboratory (first flight was STS-59 in April), part of NASA’s Mission to Planet Earth. Flying SRL during different seasons allowed comparison of changes between first and second flights. SRL-2 was activated on flight day one, and around-the-clock observations conducted by astronauts split into two teams. Besides repeating data takes over same locations as on first flight, unusual events also imaged, including erupting volcano in Russia and islands of Japan after earthquake there. Also tested was ability of SRL-2 imaging radars, Spaceborne Imaging Radar-C (SIR-C) and X- band Synthetic Aperture Radar (X-SAR), to discern difference between such human-induced phenomena as an oil spill in the ocean and naturally occurring film.

Mission also took advantage of opportunity to study fires set in British Columbia, Canada, for forest management purposes. Special readings were taken with another SRL element, Measurement of Air Pollution from satellites (MAPS), to gain better understanding of carbon monoxide emissions from burning forest. Flying for fourth time on the shuttle, MAPS is designed to measure global distribution of carbon monoxide.

On flight day six, mission extended one day by Mission Management Team. The maneuvering capability of the orbiter was demonstrated anew in the latter half of mission, when different data-gathering method was tried. Called interferometry, it required repeated, nearly coincidental imaging passes with SIR-C/X-SAR over target sites. In one instance, Endeavour piloted to within 30 feet (nine meters) of where it was flown on first flight in April. Collected data can be transcribed into detailed topographic images showing elevation and other features. Interferometric passes completed over central North America, Amazon forests of central Brazil, and volcanoes of Kamchatka Peninsula in Russia. Such images, if produced regularly over long term, could provide information on the movements of Earth’s surface as small as fraction of an inch, which could be invaluable in detecting pre-eruptive changes in volcanoes and movements in fault lines before earthquakes.

Other cargo bay payloads included five Get Away Specials (GAS): two sponsored by university student groups, one by Swedish Space Corp., and two by U.S. Postal Service holding 500,000 commemorative stamps honoring 25th anniversary of Apollo 11.

Middeck payloads: Commercial Protein Crystal Growth (CPCG) to study dynamics of protein crystallization and also to obtain protein crystals large enough to allow structural analysis; Biological Research in Canisters (BRIC-01), flying for first time and holding gypsy moth eggs to determine how microgravity affects moth development; CHROMEX-05, fifth in series designed to examine effects of microgravity on physiological processes in plants. Previous CHROMEX flights have shown that plants grown in space may not produce seed embryos; CHROMEX-05 designed to show whether infertility is due to microgravity or another environmental factor. Also in middeck: Cosmic Radiation Effects and Activation Monitor (CREAM), to collect data on cosmic rays; and Military Applications of Ship Tracks (MAST), part of five-year Navy effort to study effects of ships on marine environment.

Problems included a missing tile around overhead window; suspect temperature sensor on the orbiter Reaction Control System (RCS) vernier thruster, which led to temporary cessation of SRL-2 radar observations; and failed primary RCS thruster.

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