RocketSTEM Issue #12 - July 2015 | Page 13

the shelf and cut it to the right size, rolled it into a cylinder and then knitted the ends into a torus shape. “The 1/6 scale was perfect for the passenger, an Astronaut G.I. Joe with a silver Mercury-type space suit that I borrowed from my son. My wife and I made an Apollo backpack. She helped to sew the folding seats. The instrument panel and the steering joystick, the wire wheels with the titanium bumpers, the folding seats, the way the front and rear sections folded up and the wheels tucked in; it was all accurate, all to scale. And it was radio-controlled, so you could unfold it, sit G. I. Joe in the seat, and drive it on the floor. “GM knew I was doing it,” he continued, “but NASA was out of the loop. We were trying to sell the idea: look NASA, it’s possible to do this! We went to NASA headquarters, to Houston, and to Huntsville, and gave presentations demonstrating the model. We made a scale model of the space in which it had to fold, and showed how it worked. “In Huntsville, we pitched the engineering group. One of them, Len Bradford, led the way to von Braun’s office and he opened von Braun’s door. Instead of going in, I put the model Rover on the floor. von Braun was on the phone and the model drove in over his rug. He hung up and said, ‘What the heck is this?’ We gave him the presentation of how it worked, how it folded. The week after, he called in [NASA Project Manager] Sonny Morea, and Morea became the program manager to develop the [Rover]. “NASA issued another Request for Proposals. GM bid against Bendix for the job; it was pro forma really, because our folding and packaging design couldn’t be duplicated. We got the contract and we and Sonny Morea had just 17 months to deliver the Rover.” Specifications and pressure It was to be a spacecraft every bit as much as were the CM, the LM and the EVA suits. Morea’s office specified as absolute the requirement that “no single point failure Close-up of the LRV tire exterior, showing the woven piano wire and the titanium treads. A Delco Electronics press photo from the GM Public Relations Department states, “The mesh is steel music wire, 0.033 inched in diameter, crimped at 3/16 inch intervals, cut into 800 32-inch strands, and then woven by hand and shaped to form a tire body. The mesh, containing some 64,000 intersections of wire, is mounted to a spun aluminum disc. The herringbone tread strips are made of titanium for abrasion resistance. Inside the tire, titanium bumper rings limit deflection of the mesh as the wheel bumps on the lunar terrain.” Credit: David Clow shall abort the mission and no second failure endanger the crew,” so regardless of the deceptive simplicity of it, and the casual sense of familiarity its design and the nicknames like “Moon buggy” invited, the LRV was subject to the same inviolable standards as all the rest of the Apollo hardware. The unprecedented challenges included creating a vehicle that had to: • deploy safely in 1/6 G from the bay on the LM Descent Stage and be operable within 15 minutes or so; • operate in a vacuum with temperatures between ±250 degrees Fahrenheit; • permit ease of use by drivers wearing bulky protective suits; • cross obstacles a foot high and over two feet deep; • work without a transmission and gears, using instead four motors, one for each wheel, and operate if three of the four motors were out; • permit the operators to venture miles from, and out of sight of, the Lunar Module while still being able to return to it in the minimal time, that is, not by retracing their path but by the most direct route; • communicate via television and radio (voice and telemetry) with Houston in real time for the performance of both astronauts and the LRV, plus in support of the scientific objectives at each location visited; • protect itself from temperature extremes and dust, and dissipate its own heat; • weigh only about 450 pounds in 1G, about 75 in 1/6 G, and carry more than twice its weight; • climb grades as steep as 25 degrees, and remain stationary when parked on a grade of 45 degrees; • turn in a radius equal to its own length; • provide real-time feedback on its condition to the operators and to Mission Control; isolate faults in its batteries and take corrective action; and • deliver maximized freedom of movement for the greatest possible scientific exploration of every site. It also had to do something no spacecraft to date had done: operate without ever having been tested under actual working conditions. Its first Apollo EVA would be its shakedown cruise, over two kilometers out in the Apennines past Rhysling and Elbow, then looping back along the gaping Rima Hadley on the way 11 www.RocketSTEM .org 11