NAME: Thomas K. Mattingly II
BIRTHPLACE AND DATE: Mattingly was born March 17, 1936, in Chicago.
EDUCATION: Bachelor of Science degree in aeronautical engineering from Auburn University in 1958.
EXPERIENCE: Following graduation from college, Mattingly entered the U.S. Navy as an ensign and received his wings in 1960. He flew A-1H attack planes from the USS Saratoga from 1960 to 1963 and A-3Bís from the USS Franklin D. Roosevelt from 1964 to 1966.
He was a student at the Air Force Aerospace Research Pilot School when NASA selected him as an astronaut in April 1966. His first flight assignment was Command Module pilot on the Apollo 13 mission, but he was removed from the mission three days before the scheduled launch because he was exposed to German measles. He thereby missed the dramatic in-flight explosion and ultimately safe return of the crew. He finally flew as Command Module pilot on Apollo 16. Commander John Young, Lunar Module pilot Charles Duke, and Mattingly were launched on April 16, 1972. While Young and Duke explored the lunar surface for three days, Mattingly used instruments mounted in the service module from an altitude of 100 km to photographically and geochemically map a band of the lunar surface around the equator.
Following his return to earth, Mattingly served in astronaut managerial positions in the Space Shuttle development program. He was named to command the fourth and final test flight of the shuttle Columbia. On June 27, 1972, he and pilot Henry Hartsfield were launched on a seven-day mission during which they thoroughly tested the shuttle systems and operated the spaceplane's first military payload. Mattingly entry into space came on January 24, 1985, as commander of Discovery on the 15th shuttle flight. During three days in orbit, he and a crew of four deployed a military satellite from the cargo bay.
Thereafter he retired from NASA and the Navy, and entered the aerospace business. He worked as a Director in Grumman's Space Station Support Division. He then headed the Atlas booster program for General Dynamics in San Diego, California. At Lockheed Martin he was Vice President in charge of the X-33 development program.
NAME: Thomas K. Mattingly II (Rear Admiral, USN, Ret.)
NASA Astronaut (former)
PERSONAL DATA: Born in Chicago, Illinois, March 17, 1936. One grown son.
EDUCATION: Attended Florida elementary and secondary schools and is a graduate of Miami Edison High School, Miami, Florida; received a bachelor of science degree in Aeronautical Engineering from Auburn University in 1958.
ORGANIZATIONS: Associate Fellow, American Institute of Aeronautics and Astronautics; Fellow, American Astronautical Society; and Member, Society of Experimental Test Pilots, and the U.S. Naval Institute.
SPECIAL HONORS: Department of Defense Distinguished Service Medal (1982); NASA Distinguished Service Medals (2); JSC Certificate of Commendation (1970); JSC Group Achievement Award (1972); Navy Distinguished Service Medal; Navy Astronaut Wings; SETP Ivan C. Kincheloe Award (1972); Delta Tau Delta Achievement Award (1972); Auburn Alumni Engineers Council Outstanding Achievement Award (1972); AAS Flight Achievement Award for 1972; AIAA Haley Astronautics Award for 1973; Federation Aeronautique Internationale's V. M. Komarov Diploma in 1973.
EXPERIENCE: Prior to reporting for duty at the Lyndon
B. Johnson Space Center, he was a student at the Air Force Aerospace Research
Mattingly began his Naval career as an Ensign in 1958 and received his wings in 1960. He was then assigned to VA-35 and flew A1H aircraft aboard the USS SARATOGA from 1960 to 1963. In July 1963, he served in VAH-11 deployed aboard the USS FRANKLIN D. ROOSEVELT where he flew the A3B aircraft for two years.
NASA EXPERIENCE: Mattingly is one of the 19 astronauts
selected by NASA in April 1966.
He served as a member of the astronaut support crews for the Apollo 8 and 11 missions and was the astronaut representative in development and testing of the Apollo spacesuit and backpack (EMU).
He was designated command module pilot for the Apollo 13 flight but was removed from flight status 72 hours prior to the scheduled launch due to exposure to the German measles.
He has logged 7,200 hours of flight time -- 5,000 hours in jet aircraft.
From January 1973 to March 1978, Mattingly worked as head of astronaut office support to the STS (Shuttle Transportation System) program. He was next assigned as technical assistant for flight test to the Manager of the Orbital Flight Test Program. From December 1979 to April 1981, he headed the astronaut office ascent/entry group. He subsequently served as backup commander for STS-2 and STS-3, Columbia's second and third orbital test flights. From June 1983 through May 1984, Mattingly served as Head of the Astronaut Office DOD Support Group.
A veteran of three space flights, Mattingly has logged 504 hours in space, including 1 hour and 13 minutes of EVA (extravehicular activity) during his Apollo 16 flight. He was the command module pilot on Apollo 16 (April 16-27, 1972), was the spacecraft commander on STS-4 (June 26 to July 4, 1982) and STS 51-C (January 24-27, 1985).
Captain Mattingly resigned from NASA in 1985.
SPACE FLIGHT EXPERIENCE: Apollo 16 (April 16-27, 1972)
was the fifth manned lunar landing mission. The crew included John W. Young
(spacecraft commander), Ken Mattingly (command module pilot), and Charles M.
Duke, Jr. (lunar module pilot). The mission assigned to Apollo 16 was to collect
samples from the lunar highlands at a location near the crater Descartes. While
in lunar orbit the scientific instruments aboard the command and service module
"Casper" extended the photographic and geochemical mapping of a belt
around the lunar equator. Twenty-six separate scientific experiments were
conducted both in lunar orbit and during cislunar coast. Major emphasis was
placed on using man as an orbital observer capitalizing on the human eye's
unique capabilities and man's inherent curiosity. Although the mission of Apollo
16 was terminated one day early, due to concern over several spacecraft
malfunctions, all major objectives were accomplished through the ceaseless
efforts of the mission support team and were made possible by the most rigorous
preflight planning yet associated with an Apollo mission.
STS-4, the fourth and final orbital test flight of the Shuttle Columbia, launched from Kennedy Space Center, Florida, on June 27,1982. Mattingly was the spacecraft commander and Henry W. Hartsfield, Jr., was the pilot. This 7-day mission was designed to: further verify ascent and entry phases of shuttle missions; perform continued studies of the effects of long-term thermal extremes on the Orbiter subsystems; and conduct a survey of Orbiter-induced contamination on the Orbiter payload bay. Additionally, the crew operated several scientific experiments located in the Orbiter's cabin and in the payload bay. These experiments included the Continuous Flow Electrophoresis System experiment designed to investigate the separation of biological materials in a fluid according to their surface electrical charge. This experiment was a pathfinder for the first commercial venture to capitalize on the unique characteristics of space. The crew is also credited with effecting an in-flight repair which enabled them to activate the first operational "Getaway Special" (composed of nine experiments that ranged from algae and duckweed growth in space to fruit fly and brine shrimp genetic studies). STS-4 completed 112 orbits of the Earth before landing on a concrete runway at Edwards Air Force Base, California, on July 4, 1982.
STS-51C Discovery, the first Space Shuttle Department of Defense mission, launched from Kennedy Space Center, Florida on January 24, 1985. The crew included Ken Mattingly (spacecraft commander), Loren Shriver (pilot), Jim Buchli and Ellison Onizuka (mission specialists), and Gary Payton (DOD payload specialist). STS-51C performed its DOD mission which included deployment of a modified Inertial Upper Stage (IUS) vehicle from the Space Shuttle Discovery. Landing occurred on January 27, 1985.
Apollo 13 (AS-508) was launched from Pad A, Launch Complex 39, KSC, at 2:13 p.m. EST April 11, with astronauts James A. Lovell, Jr., John L. Swigert, Jr., and Fred W. Haise, Jr., aboard. The spacecraft and S-IVB stage entered a parking orbit with a 185.5-kilometer apogee and a 181.5-kilometer perigee. At 3:48 p.m., onboard TV was begun for five and one-half minutes. At 4:54 p.m., an S-IVB burn placed the spacecraft on a translunar trajectory, after which the CSM separated from the S-IVB and LM Aquarius. (The crew had named lunar module 7 Aquarius and CSM 109 Odyssey.) The CSM then hard-docked with the LM. The S-IVB auxiliary propulsion system made an evasive maneuver after CSM/LM ejection from the S-IVB at 6:14 p.m. The docking and ejection maneuvers were televised during a 72-minute period in which interior and exterior views of the spacecraft were also shown.
At 8:13 p.m. EST a 217-second S-IVB auxiliary propulsion system burn aimed the S-IVB for a lunar target point so accurately that another burn was not required. The S-IVB/IU impacted the lunar surface at 8:10 p.m. EST on April 14 at a speed of 259 meters per second. Impact was 137.1 kilometers from the Apollo 12 seismometer. The seismic signal generated by the impact lasted 3 hours 20 minutes and was so strong that a ground command was necessary to reduce seismometer gain and keep the recording on the scale. The suprathermal ion detector experiment, also deployed by the Apollo 12 crew, recorded a jump in the number of ions from zero at the time of impact up to 2,500 shortly thereafter and then back to a zero count. Scientists theorized that ionization had been produced by 6,300 K to 10,300 K (6,000 degrees C to 10,000 degrees C) temperature generated by the impact or that particles had reached an altitude of 60 kilometers from the lunar surface and had been ionized by sunlight.
Meanwhile back in the CSM/LM, the crew had been performing the routine housekeeping duties associated with the period of the translunar coast. At 30:40 ground elapsed time a midcourse correction maneuver took the spacecraft off a free-return trajectory in order to control the arrival time at the moon. Ensuring proper lighting conditions at the landing site. The maneuver placed the spacecraft on the desired trajectory, on which the closest approach to the moon would be 114.9 kilometers.
At 10:08 p.m. EST April 13, the crew reported an undervoltage alarm on the CSM main bus B, rapid loss of pressure in SM oxygen tank No. 2, and dropping current in fuel cells 1 and 3 to a zero reading. The loss of oxygen and primary power in the service module required an immediate abort of the mission. The astronauts powered up the LM, powered down the CSM, and used the LM systems for power and life support. The first maneuver following the abort decision was made with the descent propulsion system to place the spacecraft back in a free-return trajectory around the moon. After the spacecraft swung around the moon, another maneuver reduced the coast time back to earth and moved the landing point from the Indian Ocean to the South Pacific.
About four hours before reentry on April 17, the service module was jettisoned and the crew took photographs and made visual observations of the damaged area. About one hour before splashdown the command module was powered up and the lunar module was jettisoned. Parachutes were deployed as planned, and the Odyssey landed in the mid-Pacific 6.4 kilometers from the recovery ship U.S.S. Iwo Jima at 1:07 p.m. EST April 17. The astronauts were picked up by helicopter and transported to the recovery ship less than an hour after splashdown.
The Apollo 16 (AS-511) space vehicle was launched from Pad A, Launch Complex 39, KSC, at 12:54 p.m. EST April 16, with a crew of astronauts John W. Young, Thomas K. Mattingly II, and Charles M. Duke, Jr. After insertion into an earth parking orbit for spacecraft system checks, the spacecraft and the S-IVB stage were placed on a trajectory to the moon at 3:28 p.m. CSM transposition and docking with the LM were achieved, although a number of minor anomalies were noted.
One anomaly, an auxiliary propulsion system leak on the S-IVB stage, produced an unpredictable thrust and prevented a final S-IVB targeting maneuver after separation from the CSM. Tracking of the S-IVB ended at 4:04 p.m. EST April 17, when the instrument unit's signal was lost. The stage hit the lunar surface at 4:02 p.m. April 19, 260 kilometers northeast of the target point. The impact was detected by the seismometers left on the moon by the Apollo 12, 14, and 15 missions.
Spacecraft operations were near normal during the coast to the moon. Unexplained light-colored particles from the LM were investigated and identified as shredded thermal paint. Other activities during the translunar coast included a cislunar navigation exercise, ultraviolet photography of the earth and moon, an electrophoresis demonstration, and an investigation of the visual light-flash phenomenon noted on previous flights. Astronaut Duke counted 70 white, instantaneous light flashes that left no after-glow.
Apollo 16 entered a lunar orbit of 314 by 107.7 kilometers at 3:22 p.m. April 19. After separation of LM-11 Orion from CSM 112 Casper, a CSM active rendezvous kept the two vehicles close together while an anomaly discovered on the service propulsion system was evaluated. Tests and analyses showed the redundant system to be still safe and usable if required. The vehicles were again separated and the mission continued on a revised timeline because of the 5 3/4-hour delay.
The lunar module landed with Duke and Young in the moon's Descartes region, about 230 meters northwest of the planned target area at 9:23 p.m. EST April 20. A sleep period was scheduled before EVA.
The first extravehicular activity began at 11:59 a.m. April 21, after the eight-hour rest period. Television coverage of surface activity was delayed until the lunar roving vehicle systems were activated, because the steerable antenna on the lunar module could not be used. The lunar surface experiments packages were deployed, but accidental breaking of the electronics cable rendered the heat flow experiment inoperable. After completing activities at the experiments site, the crew drove the lunar roving vehicle west to Flag Crater, where they performed the planned tasks. The inbound traverse route was just slightly south of the outbound route, and the next stop was Spook Crater. The crew then returned via the experiment station to the lunar module and deployed the solar wind composition experiment. The duration of the extravehicular activity was 7 hours 11 minutes. The distance traveled by the lunar roving vehicle was 4.2 kilometers. The crew collected 20 kilograms of samples.
The second extravehicular traverse, which began at 11:33 a.m. April 22, was south-southeast to a mare-sampling area near the Cinco Craters on Stone Mountain. The crew then drove in a northwesterly direction, making stops near Stubby and Wreck Craters. The last leg of the traverse was north to the experiments station and the lunar module. The second extravehicular activity lasted 7 hours 23 minutes. The distance traveled by the lunar roving vehicle was 11.1 kilometers.
Four stations were deleted from the third extravehicular traverse, which began 30 minutes early at 10:27 a.m. April 23 to allow extra time. The first stop was North Ray Crater, where "House Rock" on the rim of the crater was sampled. The crew then drove southeast to "Shadow Rock." The return route to the LM retraced the outbound route. The third extravehicular activity lasted 5 hours 40 minutes, and the lunar roving vehicle traveled 11.4 kilometers.
Lunar surface activities outside the LM totaled 20 hours 15 minutes for the mission. The total distance traveled in the lunar roving vehicle was 26.7 kilometers. The crew remained on the lunar surface 71 hours 14 minutes and collected 96.6 kilograms of lunar samples.
While the lunar module crew was on the surface, Mattingly, orbiting the moon in the CSM, was obtaining photographs, measuring physical properties of the moon and deep space, and making visual observations. Essentially the same complement of instruments was used to gather data as was used on the Apollo 15 mission, but different areas of the lunar surface were flown over and more comprehensive deep space measurements were made, providing scientific data that could be used to validate findings from Apollo 15 as well as add to the total store of knowledge of the moon and its atmosphere, the solar system, and galactic space.
The LM lifted off from the moon at 8:26 p.m. EST April 23, rendezvoused with the CSM, and docked with it in orbit. Young and Duke transferred to the CSM with samples, film, and equipment, and the LM was jettisoned the next day. LM attitude control was lost at jettison; therefore a deorbit maneuver was not possible and the LM remained in lunar orbit, with an estimated orbital lifetime of about one year.
The particles and fields subsatellite was launched into lunar orbit and normal system operation was noted. However, the spacecraft orbital shaping maneuver was not performed before ejection and the subsatellite was placed in a non-optimum orbit that resulted in a much shorter lifetime than the planned year. Loss of all subsatellite tracking and telemetry data on the 425th revolution (May 29) indicated that the subsatellite had hit the lunar surface.
The mass spectrometer deployment boom stalled during a retract cycle and was jettisoned before transearth injection. The second plane-change maneuver and some orbital science photography were deleted so that transearth injection could be performed about 24 hours earlier than originally planned.
Activities during the transearth coast phase of the mission included photography for a contamination study for the Skylab program and completion of the visual light-flash-phenomenon investigation that had been partially accomplished during translunar coast. A 1-hour 24-minute transearth extravehicular activity was conducted by command module pilot Mattingly to retrieve the film cassettes from the scientific instrument module cameras, inspect the equipment, and expose a microbial-response experiment to the space environment. Two midcourse corrections were made on the return flight to achieve the desired entry interface conditions.
Entry and landing were normal, completing a 265-hour 51-minute mission. The command module was viewed on television while dropping on the drogue parachutes, and continuous coverage was provided through crew recovery. Splashdown was at 2:44 p.m. EST April 27 in mid-Pacific, 5 kilometers from the recovery ship U.S.S. Ticonderoga. All primary mission objectives had been achieved.
Deep space retrieval of film cartridges from Service Module.
Manned two crew. Fourth space shuttle test flight. Payloads: Induced Environment Contamination Monitor (IECM), Monodisperse Latex Reactor (MLR), Continuous Flow Electrophoresis System (CFES), Development Flight Instrumentation (DFl), Orbiter Experiments (OEX), first NASA getaway special (GAS), Night/Day Optical Survey of Lightning (NOSL) experiment, Vapor Phase Compression (VPC) freezer heat exchanger dynamics for freezing samples, Aerodynamic Coefficient Identification Package (AClP) experiment.
Planned Department of Defense shuttle mission. Cancelled due to payload delays.
Planned Department of Defense shuttle mission. Cancelled due to IUS failure.
Manned five crew. Deployed USA 8 (Aquacade ELINT spacecraft). Orbits of Earth: 48. Landed at: Runway 15 at Kennedy Space Center, Florida. Landing Speed: 342 kph. Touchdown miss distance: 839.00 m. Landing Rollout: 2,240.00 m. Payloads: Department of Defence classified payloads.