NAME: Jack R. Lousma
BIRTHDATE AND PLACE: Lousma was born February 29, 1936, in Grand Rapids, Michigan.
EDUCATION: Lousma received a Bachelor of Science degree in aeronautical engineering from the University of Michigan in 1959 and a degree of aeronautical engineer from the U.S. Naval Postgraduate School in 1965.
EXPERIENCE: Lousma became a Marine Corps officer in 1959 and received his flight wings a year later at the U.S. Naval Air Training Command. He served with the 2nd Marine Air Wing as an attack pilot and with the 1st Marine Wing based in Japan. He was a reconnaissance pilot with the 2nd Marine Air Wing, flying out of Cherry Point, North Carolina, when NASA selected him as one of 19 new astronauts in April 1966.
Lousma served as Command Module Pilot for the second manned Skylab mission, Skylab 3, launched on July 28, 1973. The other crew members were Commander Alan Bean and Science Pilot Owen K. Garriott. They would spend 59 days aboard the space workshop. Lousma conducted two space walks during the mission. On the tenth day of the mission, he and Garriott conducted an EVA, replacing film in the external solar telescope and erecting a second sun shade over the area of the station where a protective heat shield had ripped away during launch. On the second EVA, with Garriott, the telescope film was again changed out. During the course of the mission Earth resources photography, solar astronomy, metals processing and biological experiments were conducted.
Lousma returned to space March 22, 1982, as Commander of the third flight of the Space Shuttle. During eight days in orbit, he and Pilot Gordon Fullerton exposed the shuttle to extremes in thermal stress, tested the craft's 16 m long robot arm, and conducted science experiments. Because of bad weather at the prime landing site at Edwards Air Force Base, California, Lousma flew the shuttle to its only landing at a high altitude backup landing site at White Sands, New Mexico, on March 30.
Thereafter Lousma retired from NASA and the Marine Corps, and became an official of The Diamond General Corporation.
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.
Continued maintenance of the Skylab space station and extensive scientific and medical experiments. Installed twinpole solar shield on EVA; performed major inflight maintenance; doubled record for length of time in space. Completed 858 Earth orbits and 1,081 hours of solar and Earth experiments; three EVAs totalled 13 hours, 43 minutes.
The space vehicle, consisting of a modified Apollo command and service module payload on a Saturn IB launch vehicle, was inserted into a 231.3 by 154.7 km orbit. Rendezvous maneuvers were performed during the first five orbits as planned. During the rendezvous, the CSM reaction control system forward firing engine oxidizer valve leaked. The quad was isolated. Station-keeping with the Saturn Workshop began approximately 8 hours after liftoff, with docking being performed about 30 minutes later.
Installed second sunshade. Replaced solar camera film cartridges. During EVA by crew members of Skylab 3, a twin-boom sunshade, developed by MSFC, was deployed over the parasol of the OWS. A redesigned and refined thermal parasol had been launched with Skylab 3. However, its use would have required jettisoning the parasol deployed by crew members of Skylab 2, with the possibility of creating the same thermal problems that existed on the OWS prior to the parasol deployment. Following erection of the twin-pole sunshade, the cabin temperature stayed at a comfortable 293-297 K (67.7°F-74.9°F).
Replaced solar camera film cartridges; installed replacement gyroscopes.
Apollo 20 was originally planned in July 1969 to land in Crater Copernicus, a spectacular large crater impact area. Later Copernicus was assigned to Apollo 19, and the preferred landing site for Apollo 20 was the Marius Hills, or, if the operational constraints were relaxed, the bright crater Tycho. The planned December 1972 flight was cancelled on January 4, 1970, before any crew assignments were made. Work was stopped on LM-14; CSM-115A was studied for use on a second Skylab mission; Saturn V 515 was earmarked for use on Skylab. The remaining Apollo missions were stretched out to six-month intervals, which would have placed the Apollo 20 flight in 1974 had it not been cancelled. No crew was formally selected, but in the normal three-mission-ahead crew rotation, and with the assignments at that time, the Conrad crew would have been named. Instead they were transferred to the Skylab program. At one time it was considered possible that Mitchell would command the crew in place of Conrad. But it has also been stated that since both Conrad and Mitchell had been on the lunar surface, Stuart Roosa would have been commander. Astronaut Lind was considered by Slayton as next in line for a chance to land as lunar module pilot, but not until the never-funded Apollo 21.
This flight marked the culmination of the Apollo-Soyuz Test Project, a post-moon race 'goodwill' flight to test a common docking system for space rescue. 15 July 1975 began with the flawless launch of Soyuz 19. Apollo followed right on schedule. Despite a stowaway - a 'super Florida mosquito' - the crew accomplished a series of rendezvous manoeuvres over the next day resulting in rendezvous with Soyuz 19. At 11:10 on 17 July the two spacecraft docked. The crew members rotated between the two spacecraft and conducted various mainly ceremonial activities. Stafford spent 7 hours, 10 minutes aboard Soyuz, Brand 6:30, and Slayton 1:35. Leonov was on the American side for 5 hours, 43 minutes, while Kubasov spent 4:57 in the command and docking modules.
After being docked for nearly 44 hours, Apollo and Soyuz parted for the first time and were station-keeping at a range of 50 meters. The Apollo crew placed its craft between Soyuz and the sun so that the diameter of the service module formed a disk which blocked out the sun. This artificial solar eclipse, as viewed from Soyuz, permitted photography of the solar corona. After this experiment Apollo moved towards Soyuz for the second docking.
Three hours later Apollo and Soyuz undocked for the second and final time. The spacecraft moved to a 40 m station-keeping distance so that the ultraviolet absorption (UVA MA-059) experiment could be performed. This was an effort to more precisely determine the quantities of atomic oxygen and atomic nitrogen existing at such altitudes. Apollo, flying out of plane around Soyuz, projected monochromatic laser-like beams of light to retro-reflectors mounted on Soyuz. On the 150-meter phase of the experiment, light from a Soyuz port led to a misalignment of the spectrometer, but on the 500-meter pass excellent data were received; on the 1,000-meter pass satisfactory results were also obtained.
With all the joint flight activities completed, the ships went on their separate ways. On 20 July the Apollo crew conducted earth observation, experiments in the multipurpose furnace (MA-010), extreme ultraviolet surveying (MA-083), crystal growth (MA-085), and helium glow (MA-088). On 21 July Soyuz 19 landed safely in Kazakhstan. Apollo continued in orbit on 22-23 July to conduct 23 independent experiments - including a doppler tracking experiment (MA-089) and geodynamics experiment (MA-128) designed to verify which of two techniques would be best suited for studying plate tectonics from earth orbit.
After donning their space suits, the crew vented the command module tunnel and jettisoned the docking module. The docking module would continue on its way until it re-entered the earth's atmosphere and burned up in August 1975. Apollo splashed down about 7,300 meters from the recovery ship New Orleans. However the flight of the last Apollo spacecraft was marred by the fact that the crew almost perished while the capsule was descending under its parachute.
A failure in switchology led the automatic landing sequence to be not armed at the same time the reaction control system was still active. When the Apollo hadn't begun the parachute deployment sequence by 7,000 metres altitude, Brand hit the manual switches for the apex cover and the drogues. The manual deployment of the drogue chutes caused the CM to sway, and the reaction control system thrusters worked vigorously to counteract that motion. When the crew finally armed the automatic ELS 30 seconds later, the thruster action terminated.
During that 30 seconds, the cabin was flooded with a mixture of toxic unignited propellants from the thrusters. Prior to drogue deployment, the cabin pressure relief valve had opened automatically, and in addition to drawing in fresh air it also brought in unwanted gases being expelled from the roll thrusters located about 0.6 meter from the relief valve. Brand manually deployed the main parachutes at about 2,700 meters despite the gas fumes in the cabin.
By the time of splashdown, the crew was nearly unconscious from the fumes, Stafford managed to get an oxygen mask over Brand's face. He then began to come around. When the command module was upright in the water, Stafford opened the vent valve, and with the in-rush of air the remaining fumes disappeared. The crew ended up with a two-week hospital stay in Honolulu. For Slayton, it also meant the discovery of a small lesion on his left lung and an exploratory operation that indicated it was a non-malignant tumour.
In late 1977 shuttle orbital missions were due to start in 1979. The orbiting Skylab space station was not expected to decay until 1983. A plan to save Skylab was developed. In Phase 1a small Skylab Reboost Module would be docked to Skylab on the second Shuttle flight. This would boost the station to a higher orbit for later use, and also provide the capability of deorbiting the station into empty ocean if the decision was taken to abandon it. Astronauts Haise and Lousma were selected for this flight, and development of the reboost module was begun. But it was not to be. Aside from intense resistance from some factions at NASA headquarters, higher solar activity resulted in heavier than predicted drag on Skylab. The shuttle program also was hit with delays. Before the first shuttle flew, Skylab burned up in the atmosphere and crashed into the Australian outback on July 11, 1979.
Manned two crew. Payloads: Office of Space Science (OSS) experiments, Monodisperse Latex Reactor (MLR), Electro-phoresis Verification Test (EEVT), Plant Lignification Experiment. First and only landing by a shuttle at White Sands, New Mexico, after weather at Edwards did not permit landing there.