[FONT=Verdana, sans-serif]Ok, the last chapter was a bit weird, admittedly. Time for more serious matters.
[/FONT]ON THE SHOULDERS Of APOLLO, PART 5
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"The San Fransico event impacted (pun intended) the life of planetary scientist Eugene Merle Shoemaker. It was him who led the charge, the [/FONT][FONT=Verdana, sans-serif]Icarus[/FONT][FONT=Verdana, sans-serif] report under his arm..." [/FONT]
[FONT=Verdana, sans-serif]"With Leonor Helin and using the Palomar 48 inch reflector Shoemaker found that 1566 Icarus had shed some big fragments, making the Arietids more menacing. The San Fransisco impact happened during the meteor shower peak mid June. Another debris had a mostly similar trajectory, and it was bigger." [/FONT]
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[FONT=Verdana, sans-serif]"The debris was just big enough and his trajectory close enough from Earth to cause some worries. Shoemaker was adamant the chance of impact was minimal, but he felt ground-based observations were not precise enough. An in situ close up flyby was needed, but there were not many space probes on the pad that could be hijacked. Mariner 5, Venera 4 and an unfortunate twin Cosmos 167 had left (or failed to left) Earth for Venus only days or weeks before the impact.
At the end of June 1967 when meeting Alex Kosygin at Glassboro, President Johnson nonetheless inquired about Soviet space probes – could a Venera lander be hijacked to Icarus offspring ? But Kosygin answer was nothing could be ready before early 1968 at best. The last option left was Lunar Orbiter 5, to be launched early August 1967. And so it was. [/FONT]
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[FONT=Verdana, sans-serif]"The most desirable option" Gene Shoemaker said to the worried men standing in the Oval Office that day of July 1967 "would be to rendezvous with Icarus when it reached aphelion—the slowest point in its orbit—in November 1967. At that point it would be easiest to rendezvous with the asteroid and easiest to exert force to change its orbit. [/FONT]
[FONT=Verdana, sans-serif]But such a mission would have to be launched in spring 1967, and so it was out of the question. The MIT group quickly determined that no rockets could conceivably be readied before 1968 and this greatly constrained their options.
A slow rendezvous, or even a soft landing, is totally out of the question: Icarus would be moving too fast by 1968 for a spacecraft to reach it and then reverse direction for a rendezvous.
The only option was a fast intercept—fly out to Icarus and detonate a bomb near the surface to change its course. In this case the best way to get the most payload to Icarus would be to launch two modified Saturn V rockets into orbit. These would rendezvous with an Apollo “space tug” launched atop a Titan III rocket. The space tug would connect up the modified S-IVB third stages from the Saturns. They would then be used to push a relatively large spacecraft out to Icarus where it would detonate a large nuclear weapon. But there are many problems with this proposal.
The Saturn S-IVB third stages are not designed to carry fuel in orbit for more than six hours and would require extensive modification. A spacecraft would also have to be designed form scratch and built in under a year. Most importantly, the on-orbit operations required to link up the large craft were extensive and unproven. There would be no way to practice. This plan was rejected.[/FONT]
[FONT=Verdana, sans-serif]"What the group ultimately decided to do was to take six Saturn V rockets then in production, and with only minimal modifications to their payloads use them to carry smaller bombs to Icarus. The first launch would have to take place by April 1968, only a year away, and five more launches would have to follow at two-week increments." [/FONT]
[FONT=Verdana, sans-serif]"So there goes the Apollo program ?" the President asked dryly. [/FONT]
[FONT=Verdana, sans-serif]"Nope. Whatever happened, Icarus won't slam into the planet, not in year, never. Unfortunately the asteroid spanned some offsprings. We already knew about the Arietids for a long time; they are usually harmless. But that situation changed. Considering Icarus size, it probably didn't spanned much larger rocks. Still, now we have one on a collision course with us..." [/FONT]
[FONT=Verdana, sans-serif]"Are we doomed ?"[/FONT]
[FONT=Verdana, sans-serif]"Nope. The chance of it ever colliding with Earth are minimal. Listen. Saturn V S-IVB has been build to push the CSM-LM stack out of Earth gravity well, all 100 000 ponds of it. There's no reason a Saturn V couldn't push an equal amount of conventional explosives in the direction of the threatening asteroid, which is much smaller than Icarus itself."
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[FONT=Verdana, sans-serif]"Only three decades later was the secret protocol revealed; that is, the US military had modified a couple of Titan II 9 Mt W53 warheads to be carried aboard Saturn 501. Although that rocket maiden flight was perfect, Saturn 502, launched on April 4 1968, was by contrast a rocky flight. The mind shudder at the thinking of megatonic warheads riding that balky booster, which S-IVB was so shaken and battered it failed to restart. The nukes would have been stranded into Earth orbit !" [/FONT]
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[FONT=Verdana, sans-serif]"Lunar Orbiter 5 has been officially re-programmed from the Moon to Icarus fragment. In turn this mean that, to achieve complete coverage of the lunar surface for Apollo, the backup Lunar Orbiter 6 that was canned by NASA in April will return to the flight manifest. Yet scientists complain that if coverage is to be achieved then science will be neglected once again. They ask for more Lunar Orbiter probes, but the program has already be wound down a while back.
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[FONT=Verdana, sans-serif]December 24, 1968 [/FONT]
[FONT=Verdana, sans-serif]Public Affairs Officer
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"This is Apollo Control Houston, we estimate another 7 or 8 minutes before Apollo 8 Command and Service Module will separate from the S-IVB. We have not heard from the crew in the last few minutes, they're busy doing post TLI duties and we are looking at data here and everything we see is quite comforting. That is the next major event, separation from the booster, three hours and twenty minutes into a historical flight..."
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003:20:28 Collins:Roger. We have you about 30 seconds prior to separation, and everything's looking good.[/FONT]
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003:20:33 Borman:Roger. Call you again after separation, Houston. [/FONT]
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003:20:39 Lovell :Okay, I'm coming up on 15 seconds to Sep.[/FONT]
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003:20:42 Borman:Alright.[/FONT]
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003:20:45 Lovell:10 seconds to go.[/FONT]
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003:20:48 Anders:You in Auto?[/FONT]
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003:20:50 Borman:Yes, Auto, Auto, right.[/FONT]
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003:20:52 Anders:Okay, at zero, turn Hand Controller counter-clockwise, plus-X, and hold. [/FONT]
[FONT=Verdana, sans-serif]Jim Lovell occupied the left-hand seat and has access to the Translation Hand Controller. By turning the controller and pushing it forward, he fired the plus-X thrusters. When separation occurred the CSM immediately began moving away from the S-IVB. After three seconds, the vehicles separated and Lovell continued firing forward for a further five seconds.
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[FONT=Verdana, sans-serif]A complex sequence of events now unfolded without a glitch. A guillotine first severed the electrical connections between Apollo and the S-IVB; then a train of explosive cords cut the metal structure joining Apollo to the conical adapter to allow the spacecraft to come free. The conical adapter was cut into four long sections which were now only joined to the S-IVB by spring loaded partial hinges at the centre of their lower edge. Pyrotechnic thrusters, mounted within the intact portion of the adapter, forced pistons to push on the outside edge of each four section, causing them to begin rotating away from the vehicle's centreline. With the panels rotated about 45°, the hinges disengaged, allowing the springs within the hinge assembly to push the panels away.[/FONT]
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003:21:00 Anders:3 seconds, Launch Vehicle Tank Pressure indicator, zero; CM/LV Sep; Translational Contr, Neutral; plus-X, Off; TVC Servo Power 1, Off. [/FONT]
[FONT=Verdana, sans-serif]Sitting on top of the now peeled-off S-IVB, and revealed for the first time was the Secondary Payload, a passenger that replaced Grumman-not yet-ready Lunar Module. [/FONT][FONT=Verdana, sans-serif]
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003:21:37 Lovell:There's one adapter panel.[/FONT]
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003:21:39 Anders:After this camera [garble].[/FONT]
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003:21:46 Borman:Man, where's the S-IVB? Anybody see it, now?[/FONT]
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003:21:49 Lovell:There it is![/FONT]
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003:21:50 Borman:You found it?[/FONT]
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003:21:51 Lovell:Right in the middle. Right in the middle of my window. There's not a panel around.[/FONT]
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003:21:55 Borman: What a view![/FONT]
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003:21:58 Collins: Looks pretty good, huh?[/FONT]
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003:21:58 Lovell:Give me the camera.[/FONT]
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003:21:59 Anders:Well, we've got some still pictures we can take...[/FONT]
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003:22:01 Lovell:Could you pitch a little more?[/FONT]
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003:22:02 Borman:Yes.[/FONT]
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003:22:03 Anders:We haven't got in here, yet.[/FONT]
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003:22:12 Anders: We've Separated Houston. We got the S-IVB and its payload, right in sight.[/FONT]
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003:22:16 Capcom Michael Collins: Roger, Apollo 8. [/FONT]
[FONT=Verdana, sans-serif]Jim Lovell turned the camera toward the payload stuck to the S-IVB, puzzled. There should have been a ballast there, a big chunk of instrumented metal called the Lunar-Module Test Article, or LTA. With Grumman Lunar Module still two months in the future NASA engineers would have had to fly the Saturn V with only the load of the Apollo on top. And they disliked that, for good reasons. [/FONT]
[FONT=Verdana, sans-serif]By contrast with a near perfect maiden launch, Saturn V second flight, coincidentally set the very day Martin Luther King had been assassinated - April 4, 1968 - had been an utter disaster. The booster had suffered violent vibrations in flight, nearly tearing itself apart, shaking over its whole length like a pogo stick, with disastrous results.
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[FONT=Verdana, sans-serif]Engines had shut down with pieces of the booster skin falling apart; astronauts would certainly have been injured had the flight been manned. For a moment it looked as if the next Saturn V would have to be flown unmanned again. Marshall's position after that had been that the Saturn control system was extremely sensitive to payload weight; von Braun engineers feared any change in the established weights might bring the destructive pogo back.
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[FONT=Verdana, sans-serif]So further ballast was required to bring the payload's mass towards a figure that the launch vehicle's control system could handle. In simple English, a payload of seven tons had to fill the Lunar Module empty slot set below the crewed Apollo and above the S-IVB. And that was the Secondary Payload role, at least initially. Early on it had been as if a dumb chunk of metal could do the job, but soon George Low changed its mind, resulting in that payload stuck to the top of Apollo 8 S-IVB. The Lunar Mapping and Survey System was also set to replace Lunar Orbiter 5 that had been sent to the asteroid.
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[FONT=Verdana, sans-serif]Of course the once cancelled Lunar Orbiter 6 backup had been flown late 1967, but there had been a lot of tensions between the scientists that wanted it to study geology and the engineers that only cared about plotting Apollo future landing spots. As a result of the asteroid mess and Lunar Orbiter 5 hijacking there were enough gaps in the photographic coverage of the Moon surface that Apollo 8 ultimately had to carry a LMSS.
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[FONT=Verdana, sans-serif]Lovell hold on its camera: orders had been clear enough. Taking picture of the S-IVB payload was absolutely forbidden. [/FONT][FONT=Verdana, sans-serif]Those National Reconnaissance Office paranoid officers[/FONT][FONT=Verdana, sans-serif]. Lovell rolled his eyes.
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[FONT=Verdana, sans-serif]As incredible as it sounded, Apollo 8 was to carry a spy satellite - a machine straight out of a James Bond movie - around the Moon. The cynically named [/FONT][FONT=Verdana, sans-serif]Key Holes[/FONT][FONT=Verdana, sans-serif] snapped argentic pictures before the precious film was dropped into a reentry capsule. The film bucket then parachuted itself over the Pacific, where it was snapped in flight by a military cargo aircraft that brought it back to Hawaii, where it caught a flight to the United States and the NRO headquarters. [/FONT]
[FONT=Verdana, sans-serif]That cumbersome process obviously no longer worked around the Moon.
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[FONT=Verdana, sans-serif]On Christmas Day 1968, as Apollo 8 prepared to shoot out of lunar orbit in the direction of Earth, Anders opened the hatch that would someday led into the Lunar Module - and History. The Key Hole was stuck there; the powerful camera system was so heavy it massed half of a Lunar Module, a good 15 000 pounds.
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[FONT=Verdana, sans-serif]Frank Borman literally crawled into the spy satellite, where he painstakingly retrieved the film bucket. The hatch closed and the film safely tucked, the spy satellite was cast away and abandonned into lunar orbit. It would soon crash on the surface.
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(Picture from Giuseppe de Chiarra, an extremely talented artist)
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February 1969
[FONT=Verdana, sans-serif]"On behalf of President Johnson the National Space Council chaired by Vice President Hubert Humphrey carefully reviewed options from many sources - NASA internal planning documents, the President Science Advisory Council, and the National Academies Lunar and Planetary Mission Board (LPMB). [/FONT]
[FONT=Verdana, sans-serif]A host of possible options concerning manned spaceflight future have been reviewed, ranging from low Earth orbit activities, either through Apollo Aplications or advanced hardware like the space shuttle and a permanent space station; to lunar missions, once again either as an offspring of Apollo or through the establishment of a lunar base via a reusable nuclear shuttle (RNS). Attention was also given to manned planetary missions. Beside a Mars landing, the space council reviewed planetary flybys to Venus and Mars, with the eventual addition of sample return probes. [/FONT]
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The Space Council believe that ongoing lunar exploration through Apollo should continue in earnest.
We believe that the primary goal of manned space flight in the 1970’s which should be planned now is the scientific exploration of the moon, by both equipment and occasional manned landings using upgraded versions of the present Apollo system. [/FONT]
[FONT=Verdana, sans-serif]Alternatives for this choice are a commitment next year to a manned landing on Mars, which some of us believe could be carried out in the early or middle 1980’s, if sufficient effort were made; or an earth orbital space station to house perhaps six to nine men who would make occasional trips to and from Earth. [/FONT]
[FONT=Verdana, sans-serif]A great majority of the task force opposes a commitment to a manned Mars landing at this time. We believe that the space program in this second decade should not be built around a single monolithic goal on a fixed timetable. The task force also recognizes that a Mars landing in the early or middle 1980’s would require a substantial expansion of the NASA budget in the next few years. We also proposes that the space station receive further study without a binding commitment until its design and purposes are more clearly delineated and the possibilities of a radical reduction in the future of costs of transportation to orbit are more firmly established. It appears that the Apollo Applications program for manned flight, also scheduled for the 70’s might serve many of the purposes of a space station. [/FONT]
[FONT=Verdana, sans-serif]The Space Council heard, among many other guests, astrogeologist Eugene Shoemaker, who after managing the Ranger, Surveyors and Lunar Orbiter robotic programs is currently training Apollo astronauts. Learning from the June 18, 1967 event Shoemaker forged the concept of Flexible Path. Flexible Path is an innovative approach reworking Apollo Applications in the direction of asteroid exploration, with the ultimate goal of a landing on asteroid Eros in the year 1975.
In preparation of that landing, Apollo Applications would focuse on a) long duration missions using spent or dry workshops in Earth orbit and b) Apollo lunar landings to explore the Moon, including possible asteroid impacts on Earth satellite.
Unlike Earth, the Moon has no erosion to mask craters, although serious doubts remains about their origin. In the aftermath of the 1967 event it became of uttermost importance to determine whether the lunar craters are of volcanic or meteoritic origin.
If the latter hypothesis was confirmed, then it might be possible to estimate the rate of impacts over long period of time. According to Shoemaker "only a human brain can pick the most valuable rocks, the ones a robot would wheel past without noticing." [/FONT]
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September 1969
[FONT=Verdana, sans-serif]Gene Shoemaker pointed an area of the Moon. The resolution was just jaw dropping; the LMSS had imaged the lunar surface at a resolution of 10 inch, no less. [/FONT]
[FONT=Verdana, sans-serif]"This is Davy Rille. You can see a perfect alignement of craters, eleven of them. Much like every planetary scientist, I until recently believed those craters were of volcanic origin. Yet in the wake 1967 impact I asked myself whether an asteroid might have broken into various fragments that would have impacted the Moon separately. that was only a wild hypotheis, but that LMSS picture brought further interesting clues. Yet they remain unconclusive; we need boots of the ground as soon as possible." [/FONT]
[FONT=Verdana, sans-serif]Shoemaker smiled. He knew that recently another jaw dropping LMSS picture had found its way to President Johnson White House. It showed Tycho crater of [/FONT][FONT=Verdana, sans-serif]2001[/FONT][FONT=Verdana, sans-serif] fame, and clearly visible on the crater rim stood a rectangular box - not a monolith but the defunct Surveyor 7. He had used that picture to push the Planetary and Lunar Mission Board own agenda, that is, lunar science and geology [/FONT][FONT=Verdana, sans-serif]before[/FONT][FONT=Verdana, sans-serif] engineering when planning Apollo missions. [/FONT]
[FONT=Verdana, sans-serif]Shoemaker had its revenge over many years of frustrations. To think he had considered leaving Apollo altogether back ! [/FONT]