The largest rock sample ever collected

They completed their Station 1 stop at Plum and their sample collection included the largest rock sample ever collected on any Apollo lunar mission. At the urging of CapCom Tony England, Duke was asked to pick up a rock so big that Duke was incredulous. He knew England was being urged by Bill Muehlberger to collect the rock, which was right on the lip of Plum with its steeply sloped walls. With the stiff suit, Duke had difficulty bending down to pick up the 11.7 kg brute, resorting to trying to...

Multimedia

DVD 6-disc set. Spacecraft Films. www.spacecraft-films.com Apollo 16 Journey to Descartes. DVD 6-disc set. Spacecraft Films. www.space-craftfilms.com Apollo 17 The End of the Beginning. DVD 6-disc set. Spacecraft Films. www.spacecraftfilms.com In Their Own Words The Space Race. CD 7-disc set. Topics Entertainment. Renton, Washington. ISBN No. 1591502403 LUNAR ROVING VEHICLE COLLECTION, UNIVERSITY OF ALABAMA AT HUNTSVILLE The H. Louis Salmon Library at the University...

Space Exploration Proposal Documents

The Report of the National Commission on Space. Washington, D.C. 1986 Leadership and America's Future in Space. A Report to the Administrator. Dr. Sally K. Ride. August 1987. Lunar roving vehicle collection, University of Alabama 299 Report of the 90-Day Study on Human Exploration of the Moon and Mars. NASA TM-102999. Washington, D.C. November 1989. Report of the Advisory Committee On the Future of the U.S. Space Program. NASA, Washington, D.C. December 1990...

Apollo 17 Mission Overview

Apollo 17 (CSM America and LM Challenger) Saturn V 1972 December 7-19 Eugene A. Cernan Ronald E. Evans Harrison H. Schmitt 12 days 13 hours 52 minutes Landing site Taurus-Littrow Landing Coordinates 20.19 degrees North, 30.77 degrees East (Source National Space Science Data Center) APOLLO 17 MISSION REPORT EXCERPT 9.1 Lunar Roving Vehicle The lunar roving vehicle satisfactorily supported the lunar exploration objectives. Controllability was good, and no problems were experienced with steering,...

Lunar Communications Relay Unit and Ground Commanded Television Assembly

The lunar communications relay unit and ground-commanded television assembly operated for 12 hours 44 minutes during the lunar surface extra-vehicular activities. The relay unit in conjunction with the television camera was energized by up-link command for lunar module ascent television coverage and for six days of scientific lunar surface observations on a once-per-day basis until 30 April 1972. At that time, the system could not be energized by up-link command. Down-link data from the relay...

APOLLO 16 Mission Report Excerpt 81 Lunar Roving Vehicle

The lunar roving vehicle performance was good however, several system problems occurred. These problems are a. Higher-than-expected battery temperatures b. Multiple failures of instrumentation hardware c. Loss of rear fender extension d. Temporary loss of rear steering. Procedural errors resulted in the temporary loss of rear drive power and a temporary loss of all navigation displays except heading and speed. The approximate distances driven during the three extravehicular activities were 4.2,...

APOLLO 15 Mission Report Excerpt 983 Lunar Surface Mobility Systems Performance

Lunar roving vehicle The major hardware innovation for the lunar exploration phase of the Apollo 15 mission was the lunar roving vehicle. Because of geological requirements during surface traverses, time was limited for evaluating the characteristics of the vehicle. However, during the traverses, a number of qualitative evaluations were made. The following text discusses the performance, and the stability and control of Rover 1, as well as other operational considerations pertaining to the...

Apollo 15 Mission Overview

Apollo 15 (CSM Endeavour and LM Falcon) Saturn V 1971 July 26-August 7 David R. Scott James B. Irwin Alfred M. Worden Landing site Hadley-Apennine region near Apennine Mountains. Landing Coordinates 26.13224 degrees North, 3.63400 degrees East (Source National Space Science Data Center) 3 EVAs of 18 hours, 30 minutes, plus 33-minute Standup EVA. Worden also performed a 38-minute trans-Earth EVA. First mission to carry orbital sensors in service module of CSM. ALSEP deployed. Scientific payload...

Future rover requirements and missions

Among the first reports related to rovers since the announcement of the VSE was Expanding Frontiers with Standard Radioisotope Power Systems, published in January 2005. Written primarily by scientists and engineers at the Jet Propulsion Laboratory, with contribution from NASA Headquarters, this document looked at the power requirements of lunar and Martian rovers for the future. The original Lunar Roving Vehicle employed rather conventional batteries, which were adequate for the length of the...

The Vision for Space Exploration

The Lunar Roving Vehicle used on Apollo 15, 16 and 17 proved how valuable a rover could be to expanding the scope of the lunar mission and increased the level of scientific discovery this made possible. The Martian rovers Sojourner, Spirit and Opportunity proved that exploration of distant planets by robotic rovers could be of immense benefit, discovering the former presence of liquid water and how that presence influenced the formation of Mars' surface features. The Mars Science Laboratory...

Pathfinder And Sojourner

The seeds of robotic rover development for the exploration of Mars by the United States were planted decades before the first of those rovers actually rolled onto the Martian surface. The Martian rovers that made NASA so proud and rekindled in the general public a new wave of interest in the Red Planet can trace their roots to the Surveyor Lunar Roving Vehicle (SLRV). The SLRV was built under contract for the Jet Propulsion Laboratory (JPL) by General Motors' Defense Research Laboratories...

Prelaunch Activities

Flight hardware for Saturn Apollo launch vehicle SA-512, ultimately destined for Apollo 17, began arriving at the Kennedy Space Center in October 1970, with the arrival of the S-II second stage. The S-IVB third stage arrived at KSC on 21 December 1970, while the S-IC first stage arrived on 11 May 1972 and the S-IU instrument unit the following month. The Command and Service Modules (CSM) arrived at KSC in March 1972 and were placed in the altitude chamber in the Manned Spacecraft Operations...

A safe return

On 27 April, the Command Module Casper re-entered the Earth's atmosphere traveling at more than 16,000 kph. A picture-perfect splashdown marked the end of the greatest adventure in the lives of John Young, Charlie Duke and Ken Mattingly. Helicopters from the USS Ticonderoga picked up the crew and then the capsule. It was a mission all three men realized they could not surpass. The helicopter landed on the carrier, steps were rolled up to the side and the three astronauts exited and saluted. It...

Lunar dust problems

A walking traverse in this place would be terrible,'' Duke admitted. The missing fender extension was having the expected, if undesirable, effect of tossing lunar soil over them and their vehicle. We've got to get over this ridge, John, and we'll see the old LM,'' Duke assured Young. Man, I am covered from head to foot with dust. Boy, those fenders really are useful, Tony. This one we lost in the back has resulted in us being . . .'' Pretty dirty,'' Young finished. .a Double Pig-Pen,'' Duke...

Descartes is selected

On 3 June 1971, the Apollo Site Selection Board approved Descartes as the landing site for Apollo 16. That decision set into motion a series of events that ranged from mission-specific orbital mechanics and lunar landing simulation planning, to field geologic training and traverse simulations in the Grover for Young and Duke, and much more besides. As with Apollo 15, specific station stops and timelines were established for the Lunar Roving Vehicle traverses and the contingency walking...

Closing out EVA3

There were two other important tasks to perform that day before liftoff and Fendell made sure his TV camera was properly positioned to record both of them. The first of these tasks was for Scott to perform the first cancellation of a U.S. Postal Service stamp on the Moon. ''Okay. To show that our good Postal Service has deliveries any place in the universe, I have the pleasant task of canceling, here on the Moon, the first stamp of a new issue dedicated to commemorate United States'...

A spectacular discovery at Station

Scott did succeed in taking a sample from the boulder, which had a subtle green cast from an abundance of magnesium oxide present - a totally unexpected find. After collecting samples from the boulder, Scott drove the rover to a more level surface, Irwin got on, and they drove on to Spur Crater and Station 7. The crew had spent just under half-an-hour at Station 6A, but it had been a nervous time for Mission Control without any ''eyes'' to see what Scott and Irwin had to deal with there. At...

The Standup

Scott and Irwin then began going through their check list in preparation for the first - and last - EVA of its kind during the Apollo missions. The two astronauts would don their helmets and gloves, pressurize their suits, and then Scott would open the overhead hatch and remove the docking drogue assembly to perform a Standup EVA (SEVA). This was essentially a site survey to see whether the area was strewn with boulders or was clear enough to employ the Lunar Roving Vehicle. ''One of the...

The Landing Site Mission Rules And Lunar Science

Deke Slayton had announced the prime and backup crews for Apollo 15 on 26 March 1970, two weeks before the launch of Apollo 14. For the prime crew, he selected astronauts with previous backup crew or prime crew experience. David R. Scott was selected as mission Commander, Jim Irwin as Lunar Module Pilot, and Alfred Worden as Command Module Pilot. For the backup crew he named Richard F. Gordon as Commander, Jack Schmitt as Lunar Module Pilot and Vance D. Brand as Command Module Pilot. Later that...

Visual Simulation Training At Marshall Space Flight Center

During the late 1960s, a fixed-base visual simulator was developed by the Simulation Branch of the Computation Laboratory at the Marshall Space Flight Center to aid in the development of Lunar Roving Vehicle concepts prior to the eventual LRV design finally chosen. This simulator was designed to be used in conjunction with the Bendix Corporation and Boeing Company Lunar Roving Vehicle designs. The system was designed to present the driver with a reasonably accurate simulation of the lunar...

Training At The Manned Spacecraft Center Houston Texas

Astronaut training with respect to the Lunar Roving Vehicle employed some unique simulators. How could astronauts experience the performance characteristics of the Lunar Roving Vehicle operating in zg Earth's gravity In September 1970, Donald ''Deke'' Slayton, Director of Flight Crew Operations, sent a memo to the Director of the Manned Spacecraft Center in Houston outlining his recommendations for using the centrifuge at the MSC with the 1-G Trainer, with modifications to the centrifuge to...

Lrv Bound For The Moon With Apollo

When this program was all over, said Morea, although Boeing did indeed - as we suspected they might - overrun about 100 per cent on the cost, the remarkable thing was that there were but eight change orders over the entire life of the program. It was seventeen months from the time we signed the contract at Boeing to the day we delivered flight hardware - man-rated - to the Cape. I am very proud of that accomplishment, and Boeing and GM deserve a lot of the credit for stepping up to the plate...

Electrical Power Subsystem

The Lunar Roving Vehicle's Electrical Power Subsystem included two 36 VDC silver-zinc batteries, and wiring harnesses with connectors, circuit breakers, switches and meters. The batteries were engineered by Eagle Picher of Joplin, Missouri, and both minimum weight and power generation capability were the overriding parameters. The batteries used a lightweight magnesium case with a Plexiglas core, having twenty-three cells containing silver-zinc plates in a potassium hydroxide electrolyte. Each...

Mission And Eva Traverse Planning

With the selection of Taurus-Littrow as the landing site for Apollo 17, mission and EVA transverse planning commenced. The lunar mission was made up of scientific experiment deployment and geologic exploration, but there was also science and photography to be performed by the Command Module Pilot while in orbit around the Moon. Jack R. Sevier was Chairman of the Traverse Planning Subcommittee of the Science Working Panel, and was assisted by Dr. Robert. A. Parker, Apollo 17 Mission Scientist,...

Index

16mm Data Acquisition Camera (DAC), 48, 73 Ackermann steering, 39, 142 A.C. Delco Electronics Division, 46 Advanced Research Projects Agency (ARPA), 3 Aft Pallet Assembly, 178 Aldrin, Edwin, 17, 59 Allen, Joe, 75, 101 Alpha Particle X-Ray Spectrometer, 246 America Command Module, 173, 207, 209 Apollo 17 Flight Crew support Team, 189 Apollo Applications Program (AAP), 7, 10, Apollo Logistics Support System (ALSS), 5 Apollo Lunar Surface Experiments Package (ALSEP), 11, 111, 119 Apollo Lunar...

Leaving Descartes For Home

Lunar Receiving Labratory

At 171 hours and 31 minutes GET, an explosive charge fired a steel blade through the four-inch thick bundle of cables that joined the two stages electrically. More charges severed the bolts holding the stages together, and the ascent stage fired. The rover's TV camera, controlled from Houston, panned upward as it followed the ascent stage until it was out of range. Then the camera panned slowly down to the descent stage left behind. The unnerving realization hit those watching the monitor in...

Lrv Closeout

During the last weeks prior to launch, the Mobile Service Structure (MSS) was moved into position adjacent to the Saturn V using the Crawler Transporter. The MSS was an invaluable component of the Apollo launch facilities and permitted access to virtually every portion of the launch vehicle. Three days prior to launch, during the Lunar Module closeout procedures, the LRV underwent a procedure of its own. From the work platform, an access panel in the Spacecraft Lunar Module Adapter (SLA) which...

The second Lunar Grand Prix

Back at the LM, Duke got off and took the 16 mm Data Acquisition Camera from the rover in preparation for Young to perform the planned lunar Grand Prix. After the problems that plagued the 16 mm DAC on Apollo 15, the camera had received modifications to resolve the problems and prevent their occurrence on Apollo 16. Duke walked about fifty meters away and once he told Young the camera was rolling, Young began the test with a hard acceleration. Almost immediately, the LRV began rocking fore and...

Losing the fender extension

Lunar Dust Battery

Houston eliminated the Station 7 stop, so Young and Duke completed their stops at Stations 8, 9 and 10, which included Stubby Crater, rays from South Ray Crater and other parts of the Cayley Plains. Their stop at Station 8 was given one hour and with five minutes remaining, Young was finishing with Duke's sample collection bag while at the rear of the rover. Young turned to go around the back of the rover and his leg caught on the right rear fender extension, tearing it from its guide rails....

Training At The Kennedy Space Center Florida

Training for the J-missions at KSC in Florida involved the 1-G trainer in a simulated crater and boulder field near the Operations and Checkout Building, as well as indoor training with the Deployment Trainer. The 1-G trainer was used for rover equipment configuration setup. Florida had no rocks even remotely resembling what might be encountered on the Moon that might be used in training, so Jerry Sevier in the Engineering Office of the Manned Spacecraft Center in Houston contacted Gordon John...

Pressurized or unpressurized rovers

The authors of the Glenn Research Center document described in detail why a pressurized rover would one day have to be considered. Long-duration missions on the Moon and Mars would of necessity need to provide the astronauts with protection against radiation, as well as offering the advantage of operating and living in the vehicle without constantly having to wear the EVA suit. Unpressurized rovers would be ideal for single-day EVAs that would require the return to the lunar base crew module,...

Destiny at Taurus Littrow

On 21 May 1969, the crew of Apollo 10 entered their circularized orbit of 113.9 km by 109.1 km around the Moon after two Service Propulsion System burns. Aboard the Command Module (CM) Charlie Brown were mission Commander Thomas P. Stafford, CM Pilot John Young and Lunar Module (LM) Pilot Eugene Cernan. This mission was the first all up test of the Apollo spacecraft system that would eventually land on the Moon, including the Lunar Module. The stated mission of Apollo 10 was to demonstrate...

Its further away than you think

After completing their photography and sample collection along the rim of North Ray Crater and the vicinity near the rover, including several sizable white boulders. Young and Duke then set their sights on the massive boulder in the distance. But on the Moon, distances were very hard to gauge. The absence of familiar objects often seen on Earth made it very deceiving in trying to estimate either the size of surface features or the distance to them. This phenomenon was about to play itself out...

Learning to drive on the Moon

Scott then got into his seat in preparation for powering up the rover. He read off the critical amps, voltages and temperatures to Houston, reporting no amps or voltage on battery No. 2. This turned out to be an indicator problem and the rover did indeed have both batteries functioning. Irwin took the 16 mm film camera in hand and told Scott to let him know when he was ready to drive off so he could film the rover underway. Joe Allen admonished Scott to ''Buckle up for safety.'' And then Scott...

Stowage And Deployment Subsystem

Considerable thought, engineering and testing went into the development of the Lunar Roving Vehicle (LRV) Stowage and Deployment Subsystem. This subsystem design had to preclude premature deployment under the violent forces and loads that would be encountered during the Saturn V launch and potential hard LM landings on the Moon. A premature deployment inside the Saturn V or at LM landing could potentially have caused LRV and or LM structural damage and proven disastrous. Yet the system also had...

The Viking Missions

The Viking spacecraft was made up of an orbiter and a lander. Langley awarded development of the orbiter to the Jet Propulsion Laboratory in Pasadena, California, which would also be responsible for tracking and data acquisition and its Mission Control and Computing Center. Martin Marietta Aerospace in Denver, Colorado was awarded the contract to engineer and build the lander. Two Viking spacecraft would be built and NASA assigned its Lewis Research Center to procure and configure the...

Launch vehicle and spacecraft

The size and weight of the MSL and its spacecraft will require a more powerful launch vehicle than the Boeing Delta II used for the previous Mars rover missions. The entire MSL spacecraft payload is expected to be 2,800 kilograms with a heat shield spacecraft diameter of 4.5 meters. The Viking 1 and 2 landers and their orbiters were launched aboard Titan Centaur rockets with solid rocket motor boosters. The Titan IV rocket was retired in 2005 so available alternatives have been studied. The...

Teaching the astronauts to be geologists

Dave Scott Astronaut

Silver knew these astronauts had acute observation skills, but he wanted to direct their attention toward enhancing the scientific return of their missions by honing their ability not only to identify the types of rocks they might find, but also to determine how they might have been formed. Silver wanted to train them to be able to verbalize what they saw for the sake of the scientific teams back on Earth. He also recognized that the astronauts already had full plates, as far as training was...

The Mobility Subsystem

Harmonic Gear Drive Lrv

The largest subsystem of the LRV was the Mobility Subsystem, which consisted of the chassis, and the equipment and controls required to suspend, propel, brake and steer the rover. This included the forward, center and rear chassis, suspension, wheels, drive control electronics, traction drives, brakes, steering linkage, fluid dampers (shock absorbers) and the hand controller used to steer, accelerate and brake the LRV. Boeing brought in General Motors and its A.C. Electronics Defense Research...

Van Serg Crater

Their next destination on the rover was the small crater identified as Van Serg. Measuring 90 m in diameter, it was far smaller than Henry, Shakespeare and Cochise craters near the North Massif. Those craters measured hundreds of meters in diameter. Van Serg appeared to be sharply defined from orbital photographs and Cernan and Schmitt were to sample its dark mantle and sub-floor material. They drove around the southeast, subdued rim of Cochise Crater and soon spotted Van Serg. They had been...

The Night Launch Of Apollo

Days before the scheduled launch of Apollo 17, all the motel rooms in Cape Canaveral, Titusville and the surrounding small towns were booked. This last launch of Apollo brought in the news media from across the United States and from around the world. Many individuals traveled by car and motor home from as far away as California and Alaska to find any place they could park their vehicle to see the majestic Saturn V in the distance. All of them wanted to be part of this historic event. It was...

Eva3 The Last Day On The Moon

Gordon Fullerton, the Wakeup CapCom, roused Cernan and Schmitt from their sleep at 160 hours and 25 minutes GET to start the third and last day of Apollo 17's exploration of Taurus-Littrow. It was Wednesday, 13 December 1972. Throughout the entire mission, the Earth was lower to the Moon's horizon than for any other Apollo mission, and Cernan described the Earth's continents that were visible from the Lunar Module's window. Robert Parker soon came online as the CapCom for EVA preparations and...

The Lunar Roving Vehicle Request For Proposals

Early Wheel Design

Mueller, Associate Administrator for the Office of Manned Space Flight, selected the Lunar Roving Vehicle as the means Apollo astronauts would use to traverse and explore the Moon. On 26 May, the crew of Apollo 10 -Thomas P. Stafford, John Young and Eugene Cernan - splashed down in the Pacific Ocean after a completely successful mission designed to duplicate every step of Apollo 11, apart from landing on the surface. On 29 May, the Office of Manned Space Flight issued a...

Traverse Planning And Mission Geologic Training For The Jmissions

In October 1969, USGS geologist Gordon Swann submitted his proposal to NASA to be Principal Investigator on the Geology Experiment Team for Apollo 14 and 15. When Swann's proposal was accepted, he asked Gerald Schaber to be one of his co-investigators for those missions. This specifically involved traverse planning and subsequent mission geologic training and traverse map production. With the addition of the LRV for Apollo 15, traverse planning and training grew considerably. Swann asked...

Lunar Vehicle Testing At The Usgs

Moon Rover

In December 1963, Shoemaker appointed John McCauley as co-investigator for the Surveyor Lunar Roving Vehicle (SLRV). This was a small robotic vehicle about one meter long and half-a-meter wide and weighing approximately 45 kg. NASA conceived this vehicle to be soft-landed on the lunar surface, and to then, as its name stated, survey the surrounding area, take stereoscopic images and beam them back to Earth, as well as performing other functions. NASA contracted with Bendix Corporation and...

The Lunar Exploration And Science Conferences Of 1965 And 1967

In July 1965, NASA's Manned Space Science Coordinating Committee sponsored a conference in Falmouth, Massachusetts. Lasting two weeks, the Summer Conference on Lunar Exploration and Science was convened to map out a ten-year program of lunar exploration, with the emphasis on manned exploration. Working groups were formed in the areas of geology, geophysics, bioscience, geochemistry, astronomy, lunar atmospheric measurements and cartography. In a general sense, the conference looked at five...

The Boeingmarshall Space Flight Center Collaboration

The Marshall Space Flight Center had always been a very autonomous NASA center, whether it was engineering and building its own hardware in support of the Apollo program, or overseeing contractors responsible for building the hardware MSFC required. Although Boeing won the contract to build the LRV, test units and related equipment, MSFC would remain very much in Boeing's back pocket for the entire duration of the program. Marshall managers and engineers knew from GM-DRL built a -scale model of...

Apollo 17 Landing Site Selection

Deliberation on the landing site for Apollo 17 actually began during discussions regarding the landing site for Apollo 16 because the Apollo Site Selection Board (ASSB) considered the last two lunar landing missions complementary in their preference for lunar highlands. When the ASSB met on 3 June 1971 to select the Apollo 16 site, it also wanted to designate a prime site candidate for Apollo 17. The principal debate for the Apollo 16 landing site was between Descartes and Alphonsus on the...

Early rover prototypes

However, the space agency decided to cancel the SLRV program, choosing instead to rely on the forthcoming Surveyor lander missions and photography from the Lunar Orbiter probes that were scheduled for their first mission in 1966. GM's SLRV was returned to JPL and went into storage, all but forgotten. More than ten years later, the SLRV was rediscovered and restored to functionality on a shoestring budget and the reborn project became a technology testbed. The first thing to be developed was a...

The Lunar Roving Vehicle Wins The Mobility Debate

Moon Rover

As late as mid-1968, numerous contractors still held the view of using dual Saturn V launches to support extensive Apollo missions and their considerable hardware requirements. For example, in May 1968 GMDRL became AC-Electronics Defense Research Laboratories and published a presentation titled Roving Vehicles for Apollo Lunar Exploration Program. The presentation discussed the work the General Motors division had conducted and its relevant experience in the development of lunar surface...

A fender crisis averted

As Schmitt made for the deployment site, however, it would be the LRV that suffered some inadvertent damage. Instructions for the fender repair were transmitted to the Apollo 17 crew. Pages from the USGS Lunar Surface Map Package were taped together inside the Lunar Module and then clamped to the damaged fender. It worked surprisingly well. (NASA) Instructions for the fender repair were transmitted to the Apollo 17 crew. Pages from the USGS Lunar Surface Map Package were taped together inside...

The Sculptured Hills

Let me tell you, this rover is a machine. I don't know if it saw that hill we're climbing, but I did,'' Cernan commented to Houston as they drove toward the Sculptured Hills. The terrain was undulating and far from flat. Cernan stopped the rover briefly for Schmitt to take a sample from a roughly 40 m dark-rimmed crater with scattered small blocks inside the rim. These turned out to be instant rock,'' the phrase they used to describe lunar soil compacted by meteor impact. Geologically speaking,...

Books

Baldanza, Joseph and MacKinnon, Douglas Footprints The 12 Men Who Walked on the Moon Reflect on Their Flights, Their Lives, and the Future. New York Acropolis Books 1989 Beattie, Don Taking Science to the Moon Lunar Experiments and the Apollo Program. The Johns Hopkins University Press 2001. Benson, Charles D. & Faherty, William B Moonport A History of Apollo Launch Facilities and Operations. NASA History Series No. SP-4204, Washington, D.C. 1978. Benson, Michael Beyond Visions of the...

The Lunokhods Russias marvelous robotic rovers

In the fall of 1971, Apollo Lunar Roving Vehicle (LRV) thermal control engineers were applying experiences from the successful use of the first LRV during the Apollo 15 mission, and preparing for the next Moon exploration mission. A very interesting document was delivered to me as one of the LRV thermal engineers. This document was an unexpected English translation describing the Russian Lunokhod-1, Mobile Lunar Laboratory. Myself and others at NASA had been remotely following American space...

Apollo 17 Crew Selection

The cancellation of three Apollo missions and the reshuffling of the surviving missions, ending with Apollo 17, caused considerable consternation in the Astronaut Office. Eugene Cernan, Ron Evans and Joe Engle had been backup crew for Apollo 14 and, based on Deke Slayton's established crew rotation, these three would be the prime crew for Apollo 17. However, high level discussions had been taking place in Houston regarding the last crew. Johnson Space Center Director Robert Gilruth and...

Pathfinder and Sojourner design

The Mars Pathfinder program was an example of concurrent engineering under a pressing schedule and immovable budget. The whole spacecraft was, in fact, a series of complex systems, including the rover, the lander, the landing system and the cruise stage that would take the spacecraft to Mars after being launched aboard a Delta II rocket. Most of the Mars Pathfinder mission was cutting edge - it had never been done before. The landing system was a prime example. This mission would employ a...

Communications Subsystem

The Communications Subsystem comprised two equipment packages the Lunar Communications Relay Unit (LCRU) and the Ground-Commanded Television Assembly (GCTA). The LCRU included the electronic equipment enclosure at the front of the LRV, with an additional umbrella-like S-Band High-Gain Antenna and a Low-Gain Antenna. The LCRU was mounted in receptacles on the forward member of the forward chassis. The High-Gain Antenna and its stalk was mounted in a dedicated receptacle to the left of the LCRU,...

Engineering The 1g Lrv Trainer

The 1-G LRV trainer was built by GM's Delco Electronics Division in Santa Barbara. Of necessity, it had numerous differences required for operation on Earth. Whereas the LRV was designed to operate on the lunar surface having the gravity of Earth, the 1-G trainer had to, in effect, be reverse-engineered to withstand six times its originally designed load and stress parameters, and to take into account other factors. The 1-G trainer had no requirement for deployment with folding forward and rear...

Launch

At 6 00 a.m. on the morning of 16 April 1972, John Young, Charlie Duke and Ken Mattingly received the knock on their door from the flight surgeon in the crew quarters of the Manned Spacecraft Operations building. It was launch day for Apollo 16. The first order of business was the medical examination, which took half-an-hour. Then it was off to the traditional astronaut breakfast. While the prime and backup crews devoured their steak and eggs, Slayton went over the important milestones for the...

Thermal Control Subsystem

The function of the Thermal Control Subsystem (TCS) was to maintain all LRV components within specified temperature ranges during transit to and operation on the Moon. The TCS had to be engineered to function concurrently with the other subsystems of the LRV and to fit within an allocated weight limit of only 4.5 kg (10 lb). The LRV's electrical components could not be allowed to get too hot or too cold. This did not just apply to the LRV's operation on the Moon, but also had to be considered...

Checking Out The First

Once inside the O & C Building, the LRV was carefully inspected in its folded position. It was then removed from its shipping fixture using a specially designed sling hoist, placed on an inspection and test stand and securely bolted in place. The LRV was then unfolded and it underwent another series of inspections. The next week and a half was spent installing the battery simulators and checking out all of the vehicle's electrical systems, including the steering and drive mechanisms. The...

Exploring Hadley Rille

On this last EVA, the two astronauts would drive due west toward Hadley Rille, about two kilometers away. With the delays in trying to extract the core tube and getting them separated, they suspected that the traverse up to the North Complex might be eliminated, but Houston had not yet said so. In February 1971, Scott approached Jerry Schaber and asked him about where, if they had an extra hour on the surface, he would he recommend they go to explore Without hesitation, Schaber said the cluster...

The Usgs Branch Of Astrogeology

Dan Milton Usgs

In 1960, Eugene Shoemaker, one of the Survey's pre-eminent geologists, founded the Branch of Astrogeology in Menlo Park, California. Two years later, he moved the Branch's headquarters to Flagstaff, Arizona, one of the richest geologic locations in the entire United States. Flagstaff is situated at the foot of the San Francisco Peaks, a 3,850 m high dormant volcano that is surrounded by the extensive San Francisco Volcanic Field. This proved an ideal starting point for field training the...

Lunar Mobility Studies At Marshall Space Flight Center

Roving Vehicle Wheels

MSFC had been conducting lunar mobility studies since the early 1960s. The first of these was the Lunar Logistics System LLS , followed by the Mobility Laboratory MOLAB , then the Lunar Scientific Survey Module LSSM and the Mobility Test Article MTA . They were based on the premise of a dual-launch scenario using two Saturn Vs, one to deliver the crew to lunar orbit and the lunar surface and the other to carry all the equipment to sustain and transport the crew while they were there. The LLS,...