NAME: Frank Borman
BIRTHPLACE AND DATE: Borman was born in Gary, Indiana, on March 14, 1928.
EDUCATION: Borman received a Bachelor of Science degree from the U.S. Military Academy, West Point, in 1950 and a Master of Science degree from the California Institute of Technology in 1957. He completed the Harvard Business School's Advanced Management Program in 1970.
EXPERIENCE: Borman was a career Air Force office from 1950 to 1970, when he retired with the rank of colonel. He served as a fighter pilot in the Philippines, as an operational pilot and instructor with various squadrons in the United States, as an assistant professor of thermodynamics and fluid dynamics at West Point and as an experimental test pilot at the USAF Aerospace Pilot School.
NASA selected him as an astronaut in 1962. In December 1965, he and Jim Lovell spent a record 14 days in orbit aboard Gemini 7. During the flight, Gemini 6 astronauts Wally Schirra and Tom Stafford were launched and executed the first space rendezvous, with the two spacecraft manoeuvring to less than a metre of one another.
After being assigned Apollo 8, Deke Slayton offered Borman and his crew the first Lunar Landing, instead of Armstrong and Aldrin, but Borman turned him down. A last minute decision was made to send Apollo 8, only the second manned Apollo flight, into lunar orbit in order to beat the Russians. On December 21, 1968, the Apollo 8 crew of Borman, Lovell, and Anders became the first humans to reach escape velocity as their Saturn V put them on a trans-lunar trajectory. Early on Christmas Eve, the Apollo 8 command-service module braked into lunar orbit. In an unforgettable Christmas message to the world, Borman, Lovell and Anders read the story of creation from the first ten verses of the Bible's Book of Genesis, while sending a vivid televised image of the stark lunar surface rolling by below. On Christmas Day, Apollo 8's engines pushed the crew out of lunar orbit and back toward Earth to a landing in the Pacific Ocean.
After the flight Borman left NASA and the Air Force for an equally successful and much more lucrative career in business. From 1969 he served Eastern Airlines as a special adviser, and a year later he was named Vice President-Operations Group. He worked his way up the corporate ladder and by 1975 was President and Chief Operating Officer, becoming Chief Executive Officer later that year, and Chairman of the Board in 1976. He resigned from Eastern in 1986. Later he was an official of the Patlex Corporation.
The second manned and first long-duration mission in the Gemini program. Major objectives of the four-day mission were demonstrating and evaluating the performance of spacecraft systems in a long-duration flight and evaluating effects on the crew of prolonged exposure to the space environment. Secondary objectives included demonstrating extravehicular activity (EVA) in space, conducting stationkeeping and rendezvous maneuvers with the second stage of the launch vehicle, performing significant in-plane and out-of-plane maneuvers, demonstrating the ability of the orbit attitude and maneuver system (OAMS) to back up the retrorockets, and executing 11 experiments. The stationkeeping exercise was terminated at the end of the first revolution because most of the OAMS propellant allocated for the exercise had been used; further efforts would jeopardize primary mission objectives and could mean the cancellation of several secondary objectives. No rendezvous was attempted. The only other major problem to mar the mission was the inadvertent alteration of the computer memory during the 48th revolution in an attempt to correct an apparent malfunction. This made the planned computer-controlled reentry impossible and required an open-loop ballistic reentry. All other mission objectives were met. The flight crew began preparing for EVA immediately after terminating the stationkeeping exercise. Although preparations went smoothly, McDivitt decided to delay EVA for one revolution, both because of the high level of activity required and because deletion of the rendezvous attempt reduced the tightness of the schedule. Ground control approved the decision. The spacecraft hatch was opened at 4 hours 18 minutes into the flight and White exited 12 minutes later, using a hand-held maneuvering gun. White reentered the spacecraft 20 minutes after leaving it. The hatch was closed at 4 hours 54 minutes ground elapsed time. Drifting flight was maintained for the next two and one-half days to conserve propellant. The spacecraft landed in the Atlantic Ocean about 725 km east of Cape Kennedy - some 65 km from its nominal landing point. The crew boarded a helicopter 34 minutes after landing and was transported to the prime recovery ship, the aircraft carrier Wasp. Spacecraft recovery was completed at 2:28 p.m., a little more than 100 hours after Gemini 4 had been launched. Gemini 4 was the first mission to be controlled from the mission control center in Houston.
The space walk was hurriedly included after the Russian first in Voskhod 2. White seemed to have a lot more fun than Leonov and McDivitt took the pictures that came to symbolize man in space. With this flight the US finally started to match Russian flight durations.
Primary objectives of the mission were demonstrating manned orbital flight for approximately 14 days and evaluating the physiological effects of a long-duration flight on the crew. Among the secondary objectives were providing a rendezvous target for the Gemini VI-A spacecraft, stationkeeping with the second stage of the launch vehicle and with spacecraft No. 6, conducting 20 experiments, using lightweight pressure suits, and evaluating the spacecraft reentry guidance capability. All objectives were successfully achieved with the exception of two experiments lost because of equipment failure. Shortly after separation from the launch vehicle, the crew maneuvered the spacecraft to within 60 feet of the second stage and stationkept for about 15 minutes. The exercise was terminated by a separation maneuver, and the spacecraft was powered down in preparation for the 14-day mission. The crew performed five maneuvers during the course of the mission to increase orbital lifetime and place the spacecraft in proper orbit for rendezvous with spacecraft No. 6. Rendezvous was successfully accomplished during the 11th day in orbit, with spacecraft No. 7 serving as a passive target for spacecraft No. 6. About 45 hours into the mission, Lovell removed his pressure suit. He again donned his suit at 148 hours, while Borman removed his. Some 20 hours later Lovell again removed his suit, and both crewmen flew the remainder of the mission without suits, except for the rendezvous and reentry phases. With three exceptions, the spacecraft and its systems performed nominally throughout the entire mission. The delayed-time telemetry playback tape recorder malfunctioned about 201hours after liftoff, resulting in the loss of all delayed-time telemetry data for the remainder of the mission. Two fuel cell stacks showed excessive degradation late in the flight and were taken off the line; the remaining four stacks furnished adequate electrical power until reentry. Two attitude thrusters performed poorly after 283 hours in the mission. Retrofire occurred exactly on time, and reentry and landing were nominal. The spacecraft missed the planned landing point by only 10.3 km miles, touching down on December 18. The crew arrived at the prime recovery ship, the aircraft carrier Wasp, half an hour later. The spacecraft was recovered half an hour after the crew.
Far surpassing the Gemini 5 flight, Gemini 7 set a manned spaceflight endurance record that would endure for years. The incredibly boring mission, was made more uncomfortable by the extensive biosensors. This was somewhat offset by the soft spacesuits (used only once) and permission to spend most of the time in long johns. The monotony was broken just near the end by the rendezvous with Gemini 6.
It was originally planned to make a second solo flight test of the Block I Apollo CSM on a Saturn IB. This flight was referred to by everyone outside of the astronaut office as AS-205 or CSM-014. This flight was finally seen as unnecessary; the decision to cancel it came on November 16 and was officially announced on December 22, 1966; the Schirra crew instead became, briefly, the backup crew to Apollo 1 (replacing the original backup crew of McDivitt, Scott, Schweickart). After the Apollo 1 fire on January 27, 1967, the Schirra crew was assigned to Apollo 7, the first manned flight test of the new Block II Apollo CSM-101.
The third Apollo flight announced on December 22, 1966, was the Apollo E mission - a test of the Apollo lunar module in high earth orbit. The Borman crew would be launched aboard a Saturn V, and put into a very high earth orbit. In mid-1968 Collins had to leave the crew due to a medical problem, and was replaced by Lovell. By late 1968, Apollo 7 had flown the Apollo C mission, but delays with the lunar module meant that neither the D or E profile missions could be flown. In order to beat the Russians around the moon, it was decided that the E mission would be cancelled and instead Borman's crew would fly an Apollo CSM into lunar orbit. This became Apollo 8.
Apollo 8 (AS-503) was launched from KSC Launch Complex 39, Pad A, at 7:51 a.m. EST Dec. 21 on a Saturn V booster. The spacecraft crew was made up of Frank Borman, James A. Lovell, Jr., and William A. Anders. Apollo 8 was the first spacecraft to be launched by a Saturn V with a crew on board, and that crew became the first men to fly around the moon.
All launch and boost phases were normal and the spacecraft with the S-IVB stage was inserted into an earth-parking orbit of 190.6 by 183.2 kilometers above the earth. After post-insertion checkout of spacecraft systems, the S-IVB stage was reignited and burned 5 minutes 9 seconds to place the spacecraft and stage in a trajectory toward the moon - and the Apollo 8 crew became the first men to leave the earth's gravitational field.
The spacecraft separated from the S-IVB 3 hours 20 minutes after launch and made two separation maneuvers using the SM's reaction control system. Eleven hours after liftoff, the first midcourse correction increased velocity by 26.4 kilometers per hour. The coast phase was devoted to navigation sightings, two television transmissions, and system checks. The second midcourse correction, about 61 hours into the flight, changed velocity by 1.5 kilometers per hour.
The 4-minute 15-second lunar-orbit-insertion maneuver was made 69 hours after launch, placing the spacecraft in an initial lunar orbit of 310.6 by 111.2 kilometers from the moon's surface - later circularized to 112.4 by 110.6 kilometers. During the lunar coast phase the crew made numerous landing-site and landmark sightings, took lunar photos, and prepared for the later maneuver to enter the trajectory back to the earth.
On the fourth day, Christmas Eve, communications were interrupted as Apollo 8 passed behind the moon, and the astronauts became the first men to see the moon's far side. Later that day , during the evening hours in the United States, the crew read the first 10 verses of Genesis on television to earth and wished viewers "goodnight, good luck, a Merry Christmas and God bless all of you - all of you on the good earth."
Subsequently, TV Guide for May 10-16, 1969, claimed that one out of every four persons on earth - nearly 1 billion people in 64 countries - heard the astronauts' reading and greeting, either on radio or on TV; and delayed broadcasts that same day reached 30 additional countries.
On Christmas Day, while the spacecraft was completing its 10th revolution of the moon, the service propulsion system engine was fired for three minutes 24 seconds, increasing the velocity by 3,875 km per hr and propelling Apollo 8 back toward the earth, after 20 hours 11 minutes in lunar orbit. More television was sent to earth on the way back and, on the sixth day, the crew prepared for reentry and the SM separated from the CM on schedule.
Parachute deployment and other reentry events were normal. The Apollo 8 CM splashed down in the Pacific, apex down, at 10:51 a.m. EST, December 27 - 147 hours and 42 seconds after liftoff. As planned, helicopters and aircraft hovered over the spacecraft and pararescue personnel were not deployed until local sunrise, 50 minutes after splashdown. The crew was picked up and reached the recovery ship U.S.S. Yorktown at 12:20 p.m. EST. All mission objectives and detailed test objectives were achieved, as well as five that were not originally planned.
The crew was in excellent condition, and another major step toward the first lunar landing had been accomplished.