seemslikeadream » Mon May 12, 2014 7:00 pm wrote:[url=http://arstechnica.com/science/2014/05/did-an-impact-knock-the-moon-on-its-side/]
After eliminating a variety of areas with complex magnetic anomalies

Moderators: Elvis, DrVolin, Jeff
seemslikeadream » Mon May 12, 2014 7:00 pm wrote:[url=http://arstechnica.com/science/2014/05/did-an-impact-knock-the-moon-on-its-side/]
After eliminating a variety of areas with complex magnetic anomalies
RocketMan » Fri Oct 03, 2014 6:52 pm wrote:
This just... produces a very weird feeling in me.
I feel very weird about the going to the moon stuff. On the other hand it's the ne plus ultra of conspiracy/conspiratainment bullshit, on the other... it inspires this kind of desperate debunking which, frankly, puts me on edge.
RocketMan » Fri Oct 03, 2014 3:52 pm wrote:
This just... produces a very weird feeling in me.
I feel very weird about the going to the moon stuff. On the other hand it's the ne plus ultra of conspiracy/conspiratainment bullshit, on the other... it inspires this kind of desperate debunking which, frankly, puts me on edge.
This may be the best piece on the Apollo moon landings that I have ever read. Published by Nexxus magazine, it reads as an open letter to NASA saying "cut the bullshit already and admit that we have never been to the moon."
Is There Any Hope for a Moon Base?
by Phil Kouts PhD
The most recent of the human space flight projects, the CxP again planned to at last get to the Moon. Until its cancellation in 2010, the project had achieved remarkable progress in planning, design and early development at a cost of around US$10 billion. Yet, on 15 April 2010, President Obama – speaking to scientists, astronauts and policy makers – finally denounced the CxP. Instead of a program to return to the Moon, he outlined the plan for NASA:
"By the mid-2030s, I believe we can send humans to orbit Mars and return them safely to Earth," the President said. "And a landing on Mars will follow, and I expect to be around to see it!" (Pres. Speech, 2010)
Obviously, this totally new strategy means no landings, either on the Moon or on Mars, for at least some 20 years from 2010. So then, what is the major problem with landing on the Moon? What does it really mean in terms of technology and logistical challenges to repeat a feat which, according to the record, was confidently accomplished many times, more than 40 years ago?
The answer can be found in the latest US Government and NASA documents. Any such mission is a complex chain of essential operations all of which have to be accomplished safely. It is sufficient for one or two links in the chain to be unreliable to make a Moon return deadly dangerous, and the mission becomes absolutely impossible when just one link is incomplete. Such links were actually acknowledged by NASA.
Heat Shield of the Command Module
One crucial link in any mission to the Moon requires that the return capsule is equipped with an effective and reliable heat shield to thermally protect the craft. In particular, it was literally the vital element in the construction of each Apollo CM. This essential protection was necessary for re-entry into the Earth’s atmosphere on lunar return. The CM hits and enters the Earth’s atmosphere at the re-entry speed of 11.2 km per second (escape velocity value). Development of such a high specification shield must have been a highly significant scientific and technological challenge – especially in the mid 1960s – due to the complex technical requirements.
According to the chronology, the first successful use of the Apollo heat shield with a crew on board was in December 1968 during the return of Apollo 8 from the journey around the Moon. After that, all Apollo missions reportedly completed perfect landings and no problem has ever been highlighted or discussed.
However, the Architecture Report for the CxP reveals that NASA now does have a problem with the thermal protection material: ‘A Thermal Protection System (TPS) requires materials specifically designed to manage aero-thermal heating (heat flux, dynamic pressure) experienced during hypersonic entry, for both nominal and abort scenarios... Only ablators can meet maximum requirements; they are designed to sacrifice mass under extreme heating efficiently and reliably... The Apollo ablative TPS (AVCOAT–5061) no longer exists. Qualification of new or replacement materials will require extensive analysis and testing.’ (Arch. Study, 2005 p.629)...
... Re-entry into the Earth’s Atmosphere
Another critical link in the successful chain of operations is the choice of landing trajectory. The re-entry profile in particular determines critical requirements for the thermal shield. According to NASA, the Apollo systems performed a "direct entry", i.e. that which is along the simplest, shortest trajectory. But this choice carries with it the penalty of the maximum atmosphere resistance – resulting in maximum heat for the landing capsule and the maximum gravitational deceleration overload for a crew in the module. Another technique known as "skip entry" seems now to be preferred for returning crew modules from the Moon.
A skip entry means entering the Earth’s atmosphere with a longer gliding path and a soft bouncing on the Earth's atmosphere which allows the landing capsule to experience less heat and, at the same time, far less gravitational overload. NASA has reviewed trajectories for returning to Earth from the Moon and concludes that compared to those used during Apollo, the new concept should be implemented: ‘…it is recommended that NASA utilize skip-entry guidance on the lunar return trajectories. The skip-entry lunar return technique provides an approach for returning crews to a single ... landing site anytime during a lunar month. The Apollo-style direct-entry technique requires water or land recovery over a wide range of latitudes.’ (Arch. Study, 2005 p.39)
A wide range of latitudes would normally mean a few degrees on the globe which in turn would mean a large territory a few hundred kilometres across, which is in line with theoretical estimates for direct-entry. Strangely enough, to say that Apollo-style direct-entry requires a large territory, entirely contradicts the historical records regarding the Apollo CM splashdowns that were regularly done within a short distance from the recovery aircraft carriers. Typical splashdown miss distances of just a few kilometres were recorded for each Apollo mission recovery. Which should make the present day recovery teams very envious – as they currently pick up astronauts returning from the International Space Station (ISS) in territories dozens of kilometres across.
As a matter of fact, by mentioning "a wide range of latitudes" the modern NASA research teams denounced the declared achievement of the Apollo program in using the direct-entry technique. Today, NASA teams will have to actually develop a precise landing technique which was apparently available in the late 1960s...
...Radiation beyond Low-Earth Orbit
Regarding the radiation limits for travelling beyond LEO, ‘NASA relies on external guidance from the National Academy of Sciences and the National Council on Radiation Protection and Measurements (NCRP) for establishing dose limits. Due to the lack of data and knowledge, the NAS and NCRP recommended that radiation limits for exploration missions could not be determined until new science data and knowledge [were] obtained.’ (Arch. Study, 2005 p.109)
The next year, in swift response to NASA's request, the NCRP produced a report with a title to puzzle an unprepared reader: Information Needed to Make Radiation Protection Recommendations for Space Missions Beyond Low-Earth Orbit (NCRP, 2006). By this, the NAS admits that there is no substantial information available on cosmic radiation beyond LEO, including data on lunar surface radiation, despite the alleged achievements of Apollo.
The Augustine Committee quotes another report, this time from the National Research Council (NRC, 2008), which largely confirms the problem: 'Lack of knowledge about the biological effects of and responses to space radiation is the single most important factor limiting the prediction of radiation risk associated with human space exploration.' (Augustine, 2009, p.100)
The National Academy of Sciences needed some raw information just to be able to start working on those recommendations. Of course, some data should have been readily available to the American scientific community over the 40 years since the Apollo program.
Common sense tells us that information regarding radiation effects on the Moon, if such information exists at all, should be available within NASA, but from the Committee’s report, it is clear that NASA does not have it either. This is an incredible omission because if the Apollo crews were indeed on the lunar surface, the agency definitely should have the relevant extra-vehicular radiation data. Where is this data? Especially significant would surely be those of the Apollo 15, 16 and 17 missions.
According to the mission reports, the six astronauts on these three missions spent from 18 to 20 hours each on the lunar surface during three exits (extravehicular activities, EVAs), under the direct radiation from the Sun and other sources, in their space suits – without any additional shielding. Moreover, some EVAs occurred at the time of elevated solar activity, potentially bringing excessive solar flares or particle events and resulting radiation to the crew. It is notable that more than 40 years later, there is no overt indication that the Apollo astronauts ever experienced any residual effects from radiation exposure.
In their late 70s and early 80s, the astronauts seemingly continue to lead normal lives. Neil Armstrong recently passed away at the respectable age of 82, due to causes apparently unrelated to radiation effects. This is a fantastic outcome of the Apollo program – provided it really was accomplished in 1969-72. Yet, strangely enough, there is little indication that NASA has ever paid any attention to this remarkable bio-medical fact which is a direct scientific outcome of the Apollo program. This is important self-evident information, and NASA should have started talking about this exciting finding: that no special medical and protective precautions against walking and working on the Moon are required.
On the contrary, NASA is silent on the matter and as shown above, has asked for help on a subject where the agency should be in full possession of the prime information and be the proud leader in this research. It is also noteworthy that in its mass media releases, NASA regularly reminds its audiences about Apollo 11, where astronauts were on the surface for only two hours, while it does not usually talk about circumstances of the Apollo 12 and 14 EVAs to such a degree, and is remarkably silent on Apollo missions 15 to 17 which would be crucial evidence in favour of harmless trips to the Moon.
Regarding radiation effects on humans, the Augustine Committee concludes: 'These radiation effects are insufficiently understood and remain a major physiological and engineering uncertainty in any human exploration program beyond low-Earth orbit.' (Augustine, 2009 p.100)...
...Landing On and Taking Off from the Lunar Surface
While considering optimal strategies of travelling to the Moon and Mars, NASA admits that there could be technical problems when actually landing and thereafter taking off again from the lunar surface. The Augustine Committee considers an option to delay the Moon landing as more viable and contemplates that '[a]t least initially, astronauts would not travel into deep gravity wells of the lunar and Martian surface, deferring the cost of developing human landing and surface systems' (Augustine, 2009 p.15) – thus also avoiding any issues concerning radiation exposure during EVAs.
Nevertheless, when giving preference to a combined strategy where landing on the Moon is indefinitely delayed, the Committee admits the difficulties of developing the landing technologies. Again, why not rely on the experience apparently gained from the Apollo program? And why is a technical aspect which was so successfully handled some 40 years ago, now labelled as a "deep gravity well", implying that it is a struggle to get out of the lunar or Martian environments?
Although the Augustine Committee talks about gravity on the Moon and on Mars at the same time, one may note that the gravitational forces on the surfaces of these two space bodies are different. Let’s state it relative to our own on the Earth, in percentages: then the gravity on Mars is 37% of Earth’s, the Moon’s gravity is 16.6% or just one-sixth of Earth's. Obviously, it must be far easier to take off from the Moon.
So, one would expect NASA to discuss the comparatively greater challenge of take-off from Mars, yet the agency places both at the same level of difficulty, which seems totally illogical. In 1969 gravity wasn’t a problem for take-offs from the Moon – but for some reason by 2010 it had become a very serious problem...
... The Heavy-Launch Rocket
At the outset of the CxP in 2005, NASA put forward this recommendation: ‘Adopt and pursue a Shuttle-derived architecture as the next-generation launch system for crewed flights into LEO and for 125-mT-class cargo flights for exploration beyond Earth’s orbit. After thorough analysis of multiple ... options for crew and cargo transportation, Shuttle-derived options were found to have significant advantages with respect to cost, schedule, safety, and reliability.' (Arch. Study, 2005 p.47)
Despite these advantages, the Space Shuttle system as a key candidate had a fundamental flaw: limited payload capacity. It could hardly serve as a heavy lift vehicle for a Moon mission.
Indeed, the Saturn V allegedly used to take up to LEO a payload of approximately 120 tons, while Space Shuttle systems are limited to payloads of around 100 tons or so, including the orbiter. The redesign of these systems presents a completely new task (see below)...
...Conclusion
In April 2008, the GAO saw the key technical elements of the Apollo Space Program as a fall-back option to the system under development. However, quite possibly it was also becoming clear over time that supportive solutions were not always available from NASA’s previous experience and expertise. Whatever might be the real reasons behind this lack of will to rely upon Apollo data for matters lunar, by mid-2009, the US Government had come to realise the impossibility of completing the Constellation Program within the initially allocated timeframe of 15 years.
The GAO notes that it has reported on 'areas of technical challenge in the past, including thrust oscillation, thermal protection system ... and J-2X nozzle extension'. The GAO continues: 'In addition to these challenges, our recent work has highlighted other technical challenges, including Orion mass control, vibroacoustics, lift-off drift, launch abort system, and meeting safety requirements.' (GAO, 2009 p.10)
The GAO has identified multiple technical risks for both the launching rocket and the Orion development and, as a result, for the current mission to the Moon. Many problems identified in 2005-09 are surprisingly similar to those that would have been encountered and, of course, solved – in order for the legendary Apollo program to be successful.
The viability of the old program was inevitably questioned inside NASA when the new one started. If there wasn’t much expertise to inherit from the legendary Apollo program, then the question as to whether such a program could have been completed 40 years ago, is now highlighted in a major way. NASA still faces technical challenges which were seemingly resolved some 40 years ago. The overall message of the latest NASA reports is that the technology for journeying to the Moon is not available. Neither is a launching rocket, nor even a module for the safe transportation and return of a crew back to Earth.
Departure from the Moon’s surface, which wasn't a problem during the Apollo era, is now a problem due to the perceived difficulties in getting out of the so-called deep gravity well. Furthermore, NASA admits that the agency doesn’t have sufficient understanding of radiation beyond LEO. If just one crucial link in a Moon visitation project is missing, the whole program becomes impossible.
One such link is, certainly, the heat shield of the returning module which is still to be developed. Without an effective and reliable shield any manned lunar missions would be one way only – incapable of returning.
It was recently admitted by Tom Young, a retired Lockheed Martin executive that NASA is on "a declining trajectory". Asteroids and Lagrange points "can be steps," but do not "inspire", while there are only a few "practical" destinations – the Earth’s moon, the moons of Mars, and Mars itself. (Young, 2013) So, an idea to develop an inhabitable lunar outpost, cherished initially (Arch. Study, 2005, p. 56), still stands.
In the light of the above and many recent findings, to identify honestly the key problems and to clear the way forward to their pragmatic solution, wouldn’t it be more productive to finally recognise that the Apollo manned missions to the Moon, allegedly completed four decades ago, did not happen?
Phil Kouts
Aulis Online, June 2014
NASA Asteroid Retrieval Mission Begins to Identify Targets
WASHINGTON (NASA PR) — NASA is on the hunt to add potential candidate target asteroids for the agency’s Asteroid Redirect Mission (ARM). The robotic mission will identify, capture and redirect a near-Earth asteroid to a stable orbit around the moon. In the 2020s, astronauts will explore the asteroid and return to Earth with samples. This will test and advance new technologies and spaceflight experience needed to take humans to Mars in the 2030s.
NASA has two options for robotic asteroid capture. One concept would capture a small asteroid in its “native orbit” – the natural orbit in which it is found. The other would retrieve a boulder from a larger asteroid. NASA will decide between the capture options in December and hold a Mission Concept Review in early 2015, which will further refine the design of the mission.
A lean, agile team of NASA engineers are testing the two concepts, capitalizing on technology and engineering work already underway at NASA. Four industry teams selected through NASA’s recent Broad Agency Announcement also are developing concepts to either enhance this work or provide alternative ideas.
NASA’s plans to announce the target asteroid for the mission approximately a year before launching the robotic spacecraft, scheduled for no earlier than 2019. To date NASA has identified three valid candidates for the small asteroid concept and three for the boulder concept. The agency expects to identify one or two additional candidates each year that could become valid targets for the mission.
Before an asteroid can make the valid candidate list, NASA’s ARM target identification criteria must be met. Scientists must determine the rotation, shape, precise orbit, spectral class, and most importantly, size of the asteroid itself. With the asteroid millions of miles away from Earth, defining these factors requires a series of observations and analysis.
Telescopes on Earth and in space contribute to the observation, tracking and characterization of an asteroid. The process begins by detecting Near Earth Objects (NEOs) and starting to track their orbits. Ground observatories first scan an area in the sky to detect an object moving across the background of stationary stars and report its position in relation to them. The International Astronomical Union Minor Planet Center collects the resulting data and determines if the object has already been identified. If classified as a new object, scientists will be able to have a rough orbit and estimate of the size of the object within a day or two of the initial discovery.
Detecting an asteroid isn’t enough to conclude it could be a good candidate for NASA’s asteroid mission. Scientists need to further understand an asteroid’s shape, size, spin rate, and even surface features when picking a candidate. The best way to precisely measure these characteristics is with interplanetary radar, but only if the object is close enough to Earth to be observed this way. When the asteroid is not within the range of radar, the NASA’s Spitzer Space Telescope can contribute to the data collection using infrared imaging if the object can be seen by it.
Infrared light is a better indicator of an object’s true size because by measuring its infrared glow the amount of solar heating the entire object re-radiates can be determined. Combining the data collected by Spitzer and ground observatories allows an asteroid’s density and mass to be more precisely estimated. Spitzer’s infrared imaging has enabled NASA to determine the size of two ARM candidates thus far.
The three valid candidates so far for the small asteroid concept are 2009 BD, 2011 MD and 2013 EC20. The size of 2009 BD is estimated to be roughly 4 meters (13 feet) in size, while 2011 MD is estimated to be approximately 6 meters (20 feet). These sizes are inferred by data provided by the Spitzer observatory. 2013 EC20 is about 2 meters (7 feet) in size, as determined by radar imaging.
Most known large asteroids are too big to be fully captured and have orbits too distant for the ARM spacecraft to redirect them into orbit around the moon. Some are so distant when discovered that their size and makeup are difficult for even our most powerful telescopes to discern. Still, others could be potential candidates but go from newly discovered to out of our telescope range so quickly that there is not enough time to observe them adequately.
There are currently three validated asteroid candidates for the boulder concept, known as Itokawa, Bennu and 2008 EV5. Itokawa was well characterized by close and direct observation on the Japanese Hayabusa mission and is known to contain boulders an ideal size of roughly 3 meters (10 feet). Both 2008 EV5 and Bennu have been imaged via radar, collecting data from which it can be inferred they have boulders of the appropriate size. In addition, NASA’s OSIRIS-REx mission to launch in 2016 will study Bennu, and conduct detailed mapping of the surface of the asteroid in addition to taking samples and returning them to Earth for further study.
Any asteroid ultimately chosen for the mission will contain remnants of material from the solar system’s formation. In the 2020s, astronauts will visit the asteroid for a number of activities, including returning to Earth with substantial selected samples. The results could open new scientific learning about the formation of our solar system and the beginning of life on Earth, inform us about what resources asteroids may contain for use in future exploration, and foster partnerships with industry for future endeavors in space.
ARM will help NASA test and advance the technologies necessary for future human missions to and from Mars, including Solar Electric Propulsion, human spaceflight aboard the Orion spacecraft and the Space Launch System (SLS) rocket, and complex mission operations in deep space orbits. To learn more about ARM’s impact on the manned mission to Mars, visit How Will NASA’s Asteroid Redirect Mission Help Humans Reach Mars?
chump » Sat Oct 04, 2014 11:08 am wrote::whisper: Maybe, the moon isn't always so far away...
I saw this awhile ago on Dave McGowan's fb page:
https://www.facebook.com/WeirdScenesIns ... 7257040340This may be the best piece on the Apollo moon landings that I have ever read. Published by Nexxus magazine, it reads as an open letter to NASA saying "cut the bullshit already and admit that we have never been to the moon."
Here's a few bytes:
http://www.aulis.com/moonbase.htmIs There Any Hope for a Moon Base?
by Phil Kouts PhD
The most recent of the human space flight projects, the CxP again planned to at last get to the Moon. Until its cancellation in 2010, the project had achieved remarkable progress in planning, design and early development at a cost of around US$10 billion. Yet, on 15 April 2010, President Obama – speaking to scientists, astronauts and policy makers – finally denounced the CxP. Instead of a program to return to the Moon, he outlined the plan for NASA:
"By the mid-2030s, I believe we can send humans to orbit Mars and return them safely to Earth," the President said. "And a landing on Mars will follow, and I expect to be around to see it!" (Pres. Speech, 2010)
Obviously, this totally new strategy means no landings, either on the Moon or on Mars, for at least some 20 years from 2010. So then, what is the major problem with landing on the Moon? What does it really mean in terms of technology and logistical challenges to repeat a feat which, according to the record, was confidently accomplished many times, more than 40 years ago?
The answer can be found in the latest US Government and NASA documents. Any such mission is a complex chain of essential operations all of which have to be accomplished safely. It is sufficient for one or two links in the chain to be unreliable to make a Moon return deadly dangerous, and the mission becomes absolutely impossible when just one link is incomplete. Such links were actually acknowledged by NASA.Heat Shield of the Command Module
One crucial link in any mission to the Moon requires that the return capsule is equipped with an effective and reliable heat shield to thermally protect the craft. In particular, it was literally the vital element in the construction of each Apollo CM. This essential protection was necessary for re-entry into the Earth’s atmosphere on lunar return. The CM hits and enters the Earth’s atmosphere at the re-entry speed of 11.2 km per second (escape velocity value). Development of such a high specification shield must have been a highly significant scientific and technological challenge – especially in the mid 1960s – due to the complex technical requirements.
According to the chronology, the first successful use of the Apollo heat shield with a crew on board was in December 1968 during the return of Apollo 8 from the journey around the Moon. After that, all Apollo missions reportedly completed perfect landings and no problem has ever been highlighted or discussed.
However, the Architecture Report for the CxP reveals that NASA now does have a problem with the thermal protection material: ‘A Thermal Protection System (TPS) requires materials specifically designed to manage aero-thermal heating (heat flux, dynamic pressure) experienced during hypersonic entry, for both nominal and abort scenarios... Only ablators can meet maximum requirements; they are designed to sacrifice mass under extreme heating efficiently and reliably... The Apollo ablative TPS (AVCOAT–5061) no longer exists. Qualification of new or replacement materials will require extensive analysis and testing.’ (Arch. Study, 2005 p.629)...... Re-entry into the Earth’s Atmosphere
Another critical link in the successful chain of operations is the choice of landing trajectory. The re-entry profile in particular determines critical requirements for the thermal shield. According to NASA, the Apollo systems performed a "direct entry", i.e. that which is along the simplest, shortest trajectory. But this choice carries with it the penalty of the maximum atmosphere resistance – resulting in maximum heat for the landing capsule and the maximum gravitational deceleration overload for a crew in the module. Another technique known as "skip entry" seems now to be preferred for returning crew modules from the Moon.
A skip entry means entering the Earth’s atmosphere with a longer gliding path and a soft bouncing on the Earth's atmosphere which allows the landing capsule to experience less heat and, at the same time, far less gravitational overload. NASA has reviewed trajectories for returning to Earth from the Moon and concludes that compared to those used during Apollo, the new concept should be implemented: ‘…it is recommended that NASA utilize skip-entry guidance on the lunar return trajectories. The skip-entry lunar return technique provides an approach for returning crews to a single ... landing site anytime during a lunar month. The Apollo-style direct-entry technique requires water or land recovery over a wide range of latitudes.’ (Arch. Study, 2005 p.39)
A wide range of latitudes would normally mean a few degrees on the globe which in turn would mean a large territory a few hundred kilometres across, which is in line with theoretical estimates for direct-entry. Strangely enough, to say that Apollo-style direct-entry requires a large territory, entirely contradicts the historical records regarding the Apollo CM splashdowns that were regularly done within a short distance from the recovery aircraft carriers. Typical splashdown miss distances of just a few kilometres were recorded for each Apollo mission recovery. Which should make the present day recovery teams very envious – as they currently pick up astronauts returning from the International Space Station (ISS) in territories dozens of kilometres across.
As a matter of fact, by mentioning "a wide range of latitudes" the modern NASA research teams denounced the declared achievement of the Apollo program in using the direct-entry technique. Today, NASA teams will have to actually develop a precise landing technique which was apparently available in the late 1960s......Radiation beyond Low-Earth Orbit
Regarding the radiation limits for travelling beyond LEO, ‘NASA relies on external guidance from the National Academy of Sciences and the National Council on Radiation Protection and Measurements (NCRP) for establishing dose limits. Due to the lack of data and knowledge, the NAS and NCRP recommended that radiation limits for exploration missions could not be determined until new science data and knowledge [were] obtained.’ (Arch. Study, 2005 p.109)
The next year, in swift response to NASA's request, the NCRP produced a report with a title to puzzle an unprepared reader: Information Needed to Make Radiation Protection Recommendations for Space Missions Beyond Low-Earth Orbit (NCRP, 2006). By this, the NAS admits that there is no substantial information available on cosmic radiation beyond LEO, including data on lunar surface radiation, despite the alleged achievements of Apollo.
The Augustine Committee quotes another report, this time from the National Research Council (NRC, 2008), which largely confirms the problem: 'Lack of knowledge about the biological effects of and responses to space radiation is the single most important factor limiting the prediction of radiation risk associated with human space exploration.' (Augustine, 2009, p.100)
The National Academy of Sciences needed some raw information just to be able to start working on those recommendations. Of course, some data should have been readily available to the American scientific community over the 40 years since the Apollo program.
Common sense tells us that information regarding radiation effects on the Moon, if such information exists at all, should be available within NASA, but from the Committee’s report, it is clear that NASA does not have it either. This is an incredible omission because if the Apollo crews were indeed on the lunar surface, the agency definitely should have the relevant extra-vehicular radiation data. Where is this data? Especially significant would surely be those of the Apollo 15, 16 and 17 missions.
According to the mission reports, the six astronauts on these three missions spent from 18 to 20 hours each on the lunar surface during three exits (extravehicular activities, EVAs), under the direct radiation from the Sun and other sources, in their space suits – without any additional shielding. Moreover, some EVAs occurred at the time of elevated solar activity, potentially bringing excessive solar flares or particle events and resulting radiation to the crew. It is notable that more than 40 years later, there is no overt indication that the Apollo astronauts ever experienced any residual effects from radiation exposure.
In their late 70s and early 80s, the astronauts seemingly continue to lead normal lives. Neil Armstrong recently passed away at the respectable age of 82, due to causes apparently unrelated to radiation effects. This is a fantastic outcome of the Apollo program – provided it really was accomplished in 1969-72. Yet, strangely enough, there is little indication that NASA has ever paid any attention to this remarkable bio-medical fact which is a direct scientific outcome of the Apollo program. This is important self-evident information, and NASA should have started talking about this exciting finding: that no special medical and protective precautions against walking and working on the Moon are required.
On the contrary, NASA is silent on the matter and as shown above, has asked for help on a subject where the agency should be in full possession of the prime information and be the proud leader in this research. It is also noteworthy that in its mass media releases, NASA regularly reminds its audiences about Apollo 11, where astronauts were on the surface for only two hours, while it does not usually talk about circumstances of the Apollo 12 and 14 EVAs to such a degree, and is remarkably silent on Apollo missions 15 to 17 which would be crucial evidence in favour of harmless trips to the Moon.
Regarding radiation effects on humans, the Augustine Committee concludes: 'These radiation effects are insufficiently understood and remain a major physiological and engineering uncertainty in any human exploration program beyond low-Earth orbit.' (Augustine, 2009 p.100)......Landing On and Taking Off from the Lunar Surface
While considering optimal strategies of travelling to the Moon and Mars, NASA admits that there could be technical problems when actually landing and thereafter taking off again from the lunar surface. The Augustine Committee considers an option to delay the Moon landing as more viable and contemplates that '[a]t least initially, astronauts would not travel into deep gravity wells of the lunar and Martian surface, deferring the cost of developing human landing and surface systems' (Augustine, 2009 p.15) – thus also avoiding any issues concerning radiation exposure during EVAs.
Nevertheless, when giving preference to a combined strategy where landing on the Moon is indefinitely delayed, the Committee admits the difficulties of developing the landing technologies. Again, why not rely on the experience apparently gained from the Apollo program? And why is a technical aspect which was so successfully handled some 40 years ago, now labelled as a "deep gravity well", implying that it is a struggle to get out of the lunar or Martian environments?
Although the Augustine Committee talks about gravity on the Moon and on Mars at the same time, one may note that the gravitational forces on the surfaces of these two space bodies are different. Let’s state it relative to our own on the Earth, in percentages: then the gravity on Mars is 37% of Earth’s, the Moon’s gravity is 16.6% or just one-sixth of Earth's. Obviously, it must be far easier to take off from the Moon.
So, one would expect NASA to discuss the comparatively greater challenge of take-off from Mars, yet the agency places both at the same level of difficulty, which seems totally illogical. In 1969 gravity wasn’t a problem for take-offs from the Moon – but for some reason by 2010 it had become a very serious problem...... The Heavy-Launch Rocket
At the outset of the CxP in 2005, NASA put forward this recommendation: ‘Adopt and pursue a Shuttle-derived architecture as the next-generation launch system for crewed flights into LEO and for 125-mT-class cargo flights for exploration beyond Earth’s orbit. After thorough analysis of multiple ... options for crew and cargo transportation, Shuttle-derived options were found to have significant advantages with respect to cost, schedule, safety, and reliability.' (Arch. Study, 2005 p.47)
Despite these advantages, the Space Shuttle system as a key candidate had a fundamental flaw: limited payload capacity. It could hardly serve as a heavy lift vehicle for a Moon mission.
Indeed, the Saturn V allegedly used to take up to LEO a payload of approximately 120 tons, while Space Shuttle systems are limited to payloads of around 100 tons or so, including the orbiter. The redesign of these systems presents a completely new task (see below)......Conclusion
In April 2008, the GAO saw the key technical elements of the Apollo Space Program as a fall-back option to the system under development. However, quite possibly it was also becoming clear over time that supportive solutions were not always available from NASA’s previous experience and expertise. Whatever might be the real reasons behind this lack of will to rely upon Apollo data for matters lunar, by mid-2009, the US Government had come to realise the impossibility of completing the Constellation Program within the initially allocated timeframe of 15 years.
The GAO notes that it has reported on 'areas of technical challenge in the past, including thrust oscillation, thermal protection system ... and J-2X nozzle extension'. The GAO continues: 'In addition to these challenges, our recent work has highlighted other technical challenges, including Orion mass control, vibroacoustics, lift-off drift, launch abort system, and meeting safety requirements.' (GAO, 2009 p.10)
The GAO has identified multiple technical risks for both the launching rocket and the Orion development and, as a result, for the current mission to the Moon. Many problems identified in 2005-09 are surprisingly similar to those that would have been encountered and, of course, solved – in order for the legendary Apollo program to be successful.
The viability of the old program was inevitably questioned inside NASA when the new one started. If there wasn’t much expertise to inherit from the legendary Apollo program, then the question as to whether such a program could have been completed 40 years ago, is now highlighted in a major way. NASA still faces technical challenges which were seemingly resolved some 40 years ago. The overall message of the latest NASA reports is that the technology for journeying to the Moon is not available. Neither is a launching rocket, nor even a module for the safe transportation and return of a crew back to Earth.
Departure from the Moon’s surface, which wasn't a problem during the Apollo era, is now a problem due to the perceived difficulties in getting out of the so-called deep gravity well. Furthermore, NASA admits that the agency doesn’t have sufficient understanding of radiation beyond LEO. If just one crucial link in a Moon visitation project is missing, the whole program becomes impossible.
One such link is, certainly, the heat shield of the returning module which is still to be developed. Without an effective and reliable shield any manned lunar missions would be one way only – incapable of returning.
It was recently admitted by Tom Young, a retired Lockheed Martin executive that NASA is on "a declining trajectory". Asteroids and Lagrange points "can be steps," but do not "inspire", while there are only a few "practical" destinations – the Earth’s moon, the moons of Mars, and Mars itself. (Young, 2013) So, an idea to develop an inhabitable lunar outpost, cherished initially (Arch. Study, 2005, p. 56), still stands.
In the light of the above and many recent findings, to identify honestly the key problems and to clear the way forward to their pragmatic solution, wouldn’t it be more productive to finally recognise that the Apollo manned missions to the Moon, allegedly completed four decades ago, did not happen?
Phil Kouts
Aulis Online, June 2014
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http://www.aulis.com/moonbase2.htm
For me, the most ironic token of [the first human moon landing] is the plaque signed by President Richard M. Nixon that Apollo 11 took to the moon. It reads, ‘We came in peace for all Mankind.’ As the United States was dropping seven and a half megatons of conventional explosives on small nations in Southeast Asia, we congratulated ourselves on our humanity. We would harm no one on a lifeless rock.”
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