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By the way, my edit x button is located together on my screen and I can not delete.
Then something is probably wrong with your browser, try using a different one, Firefox is highly recommended.
When it's working properly please delete all your OT messages, they add nothing but confusion to this topic. Thanks.
Crew portrait - imaged 25 Sep 2007
From the left are astronauts Gregory E. Chamitoff, Michael E. Fossum, both STS-124 mission specialists; Kenneth T. Ham, pilot; Mark E. Kelly, commander; Karen L. Nyberg, Ronald J. Garan and Japan Aerospace Exploration Agency's (JAXA) Akihiko Hoshide, all mission specialists. Chamitoff is scheduled to join Expedition 17 as flight engineer after launching to the International Space Station
Whichever way that CME was traveling in 2007, it's too late to start running now. For the next one, the best thing to do is start digging rather than running.
Here's a clip on youtube - and more details here
There's a big difference between falling from the ISS altitude of about 400km and reentering from LEO at the same altitude - it's about a factor of 400 in energy. Soyuz takes about an hour to land after it's deorbit burn.
LEO velocity is about 8 kms/sec, all that energy has to go somewhere. Spacecraft use friction turn it into heat - LOTS of heat - so they need heavy heat shields to stop burning up.
So, add a heat shield to a spacesuit and a small deorbit propulsion unit plus a parachute etc etc and it should work, but then it's a spacecraft not a spacesuit.
Fission Surface Power (FSP) system - reference concept layout
From System Concepts for Affordable Fission Surface Power (PDF 2MB) - January 2008
NASA and DOE conducted a 12 month study to estimate the cost of a FSP system for lunar and Mars missions. Screening studies were performed to evaluate technology options and design variables before selecting a preliminary reference concept for costing. The screening studies led to a UO2-fueled, NaK-cooled reactor with Stirling power conversion and water-based heat rejection capable of providing 40 kWe with an 8 yr design life. The reference system is emplaced in a pre-excavated hole to allow nearoutpost siting and reduce radiation levels to less than 5 rem/yr at 100 m separation distance. The reactor uses stainless steel construction, limiting nominal coolant temperatures to less than 900 K, in order to minimize development cost and leverage terrestrial technology. Stirling power conversion is well suited to the operating temperature, providing high efficiency at relatively high heat rejection temperature. The use of water heat transport and water heat pipe radiator panels provides efficient waste heat removal, using a deployment approach that is derived from the ISS radiators. The FSP system concept is extensible to Mars, with materials and design strategies that are fully compatible with the Martian environment. The total system mass with 20 percent margin is less than 5000 kg.
Solar Tsunami - 7 Apr 2008
Sequences of STEREO satellite images of a solar tsunami blasting across the Sun's million degree atmosphere. Solar tsunamis are launched by huge explosions near the Sun's atmosphere, called coronal mass ejections (CMEs). These waves can travel at over a million kilometers per hour. The tsunami took place on 19th May 2007 and lasted for about 35 minutes, reaching peak speeds around 20 minutes after the initial blast.
Right. Are you sure it's not a same sex marriage?
WOT may not go away for a long time, but it's unlikely to be so expensive. Once Iraq is stabalized the cost will drop very quickly.
Hopefully the US will need not need to invade another country, with the possible exception of Iran. If it becomes necessary to remove the Mullahs there's a far more unified population to take over.
louis,
that $400 billion figure may not be so incredulous. Just returning to the Moon will cost over $100 billion, GAO estimated $230 billion but they added in ISS out to 2020. Add constructing the Outpost and supporting it for a decade and that's probably another $50 billion. Add to that the cost of the Mars robotic program and that could be another $50 billion over the next 30 years. Plus the research for human factors, high mass landing systems, reliable closed loop life support, perhaps NTP as well as the development cost of MTV and the Mars surface systems and in total there may not be much change from $400 billion.
Missions to Mars are going to be expensive in both development and operations unless some big breakthroughs happen. However spread that $400 billion over 25 years say and it's $16 billion a year, not that far away from NASA's budget today.
Gregori,
5-8 years is impossible without a national crash program like Apollo - and that only gets us back to the Moon. Mars will take longer. More than 8 years automatically means a change of president and probably two, that makes it harder but not impossible. ISS has taken 20 years and its still not compete, yet it's survived (only just) several administrations.
There will be a raw images webpage like the one available for MER, so images can be download, processed and interpreted as much you desire.
The first images will be available online from Pat Woida soon after landing (about 5pm local time), but they will be looking at the solar arrays, masts and the landing pad. So not much of the surface will be visible. PHX has to wait for the next pass of ODY/MRO before it can relay data. The so called mission success panorama, a partial 120° monochromatic image, will be sent back within the first few sols.
22 days
If McCain became president and got excited about Moon and Mars and announced a high priority program and the funding, it would enormously help. Even though Bush launched the VSE and set human exploration of Mars set as a goal, he didn't appropriate funds.
The VSE timing was bad because of the enormous cost of the WOT, yet this may change in the next few years. There's a big opportunity to convince the next president to fully support the space program. It's important that everyone pushes for this and pushes for a truly big increase in funding for the whole program, both exploration and science.
Successful Test Firing of Space Shuttle Reusable Solid Rocket Motor
MINNEAPOLIS, May 1 /PRNewswire-FirstCall/ -- The Utah desert was filled with the sight and sound of power today as Alliant Techsystems (NYSE: ATK) conducted a successful test firing of NASA's space shuttle reusable solid rocket motor (RSRM) as part of continuous testing to improve performance and ensure safety of the space shuttle and to aid development of the first stage of Ares I.
An average of 2.6 million pounds of thrust was generated during the test that lasted just over two minutes -- the same duration as when launching the space shuttle. The test included 32 objectives, with the main two being validation of the age-life certification of the motor and measuring the acoustics, or sound, emitted from the booster when it fires.
Validating the booster's age-life certification was performed by comparing it to its twin booster that was test fired three years ago. Both boosters were manufactured at the same time using the same components. They were shipped to the Kennedy Space Center and subsequently stacked then de-stacked before being returned to Utah.
The booster fired today was more than seven years old -- the oldest RSRM ever fired. Shuttle motors are currently certified to be launched for up to five years after the propellant is cast. As a result of the test, ATK and NASA engineers will better understand what effect aging and exposure to different climates have on the motors.
Another main test objective is gathering data to aid in the development of the new Ares I vehicle and its launch pad. More than 20 microphones were installed at the test site to collect information that will help predict the lift-off acoustics for Ares I. By collecting acoustic environment measurements, engineers can make better predictions of how the sound will affect the surrounding area. The shuttle program uses massive sprayers, called the water deluge system, to reduce the acoustic effects of the space shuttle propulsion systems as it lifts off. A similar system is being developed for the Ares I and data collected from this test will play an important role in the final design.
"Ground test firings provide valuable data to ensure the reliability and safety of space shuttle motors," said Ron Dittemore, president ATK Launch Systems. "The ground tests also provide critical information needed for the development of the first stage of Ares I."
It's not quite as simple as a lack political will. The political will to fast track a human Mars program is the reflection of the agendas and interests of many groups. The largest of these groups is the public, opinion polls have not shown any great interest in such a project. The public do support the space program, but they rate many other program higher, for example medical ones as well as the usual suspects: jobs, crime, education etc etc.
If the president got excited about Mars and announced a high priority program and the funding, that would do the trick. Bush has responded, that's why VSE was launched and why NASA has Mars set as a goal, however, funds were not appropriated. The timing was bad because of the enormous cost of the WOT, yet this may change in the next few years. There's a big opportunity to convince the next president to fully support the space program. It's important that everyone pushes for this and pushes for a truly big increase in funding for the whole program, both exploration and science.
To be fair the one redeeming quality of the L2 point is that its permanently in Earth's shadow, now that you mention the boil-off problem.
cIclops to Major Tom: L2 is not in Earth's shadow.
Only a small part of NASA's budget is used for true outsourcing, that is buying goods and services from non-US companies. Almost all international cooperation is done on a "no exchange of funds" basis. Flying instruments on the spacecraft of non-US agencies is a net gain as it makes more missions possible for the same amount of funding. Equally, adding non-US instruments to a US project enhances its capabilities at no cost.
Compared with the humungous cost of Federal health care and Social security, the amount of money involved in such "outsourcing" is lost in the noise. It's a red herring designed to provoke protectionism.
3 degrees north in this environment is not an excuse for change of process.
Those sites are also on opposite sides of the planet, even at 80° latitude this means they are about 1000 kms apart. Perhaps even more importantly they are two months apart in time.
(BTW messages can be deleted by clicking the little X next to the edit button)
Packaging configuration inside the Ariane 5 fairing
From A Bigger and Better Time Machine (PDF) - dated 3 Mar 2008
Well written overview of the JWST from the ESA point of view with details of their NIRSpec and MIRI instruments. NIRSpec can take spectra of up to 100 objects simultaneously!
Mobile habitat concept
From Structural Definition and Mass Estimation of Lunar Surface Habitats (PDF 11MB) - dated 14 Mar 2008
The Habitat units are landed on the lunar surface as pre-integrated units that are moved by the Lander and connected together using the Lander mobility system. All subsystems and utilities are pre-integrated into each of the Habitat units. The first PLM that lands is also on a mobile ander and is reused and retro fitted for exercise and medical operations and becomes the third unit. The Habitats remain on the mobile Landers, so they have the capability to disconnect and move the outpost to a new location.
PLM = Pressurized Logistics Module
These mobile platforms look much like ATHLETE, they would add enormous flexibility to the Outpost.
Texans in Congress try to boost NASA budget - 29 Apr 2008
By STEWART M. POWELL
Copyright 2008 Houston Chronicle Washington BureauWASHINGTON — The Texas congressional delegation pressed ahead Tuesday with an uphill, election-year effort to boost NASA's $17.3 billion budget so the space agency can close the five-year gap between retirement of the shuttle fleet and the next generation of manned spacecraft.
Twelve House members from Texas and 18 others from across the country, led by Rep. Nick Lampson, D-Stafford, urged House leaders to add $2 billion to NASA's budget. Hutchison asks $1 billion In the Senate, Kay Bailey Hutchison, R-Texas, a member of the powerful Appropriations Committee, said she was asking colleagues to add at least $1 billion to the NASA budget.
Hutchison said she wants to add one more shuttle flight in order to ferry the $1.5 billion Alpha Magnetic Spectrometer to the international space station to study the energy-producing possibilities of cosmic rays.
"We're not giving NASA the priority it should have," said Hutchison, a member of the Senate Republican leadership. "It should remain the premier agency for innovation and research."
Lawmakers are confronting a looming gap in manned U.S. spaceflight, as NASA prepares to retire the three-ship shuttle fleet in 2010 and rely on Russia's Soyuz program to ferry Americans to the space station until NASA's Orion crew exploration vehicle becomes fully operational in 2016.
"Minimizing the gap in human spaceflight, currently projected to last between 2010 and 2015, requires a national commitment, a willingness to maintain our nation's technological leadership in this field and a desire to provide the funds necessary," NASA's House supporters wrote Tuesday in a letter to Speaker Nancy Pelosi, D-Calif., Minority Leader John Boehner, R-Ohio, and four other congressional leaders.
"We believe these funds will provide an immediate and long-term economic stimulus for our nation's economy ... contributing new jobs, industrial development and stimulus to struggling communities," the lawmakers added.
Signers of the letter included all nine House members from the Houston area — four Democrats and five Republicans. The other 21 signers were all Democrats.
It's a trade off between payload mass and DV. More DV is needed to climb out of the Sun's gravity well. More DV will also reduce travel time but unless aerocapture can be made to work, more DV is needed to slow down again.
The rocket equation gives an approximate solution:
payload/initial mass = e^(-DV/3500) for LOX/LH2, DV in meters/sec
This lecture is so good it just has to be mentioned somewhere and this seems the best place. It's not about Mars, it's about the last mission to be Moon. Jack was the first and only scientist to walk on the Moon.
Lecture can be viewed or download here - video - 65 mins - 13 Mar 2008
Each post can be linked directly, just copy the link from the little symbol just in front of the "Posted: ....." date timestamp.
Assuming you are referring to this image and text, this is at 84°N 1°E whereas the image and text you refer to are at 81°N 200°E - a long way from there.
McCain recently worried space supporters by backing a plan to freeze all federal discretionary spending -- including NASA's budget -- except on defense and homeland-security programs.
McCain did say he would freeze all discretionary spending, but did he specifically mention that NASA was included or was that part fabricated by Robert Bock?
McCain should be pressed on this. As he believes the scientists that tell him there's a global warming crisis caused by burning fossil fuels, he ought to believe the NAS and space scientists that say NASA's programs are also in crisis because of a shortage of funding.
First of all over 70 percent of the Earths atmosphere, estimate, is below 0c and melting is not the primary process of phase change.
Now I posted a response to such a caption on this thread. Maybe this is not the place to respond. I challenged cIclopes about it and got ignored. That’s OK. If we just want to believe every thing we are told.Note, Your image about defrosting dunes has been changed in the April 30 release. They now acknowledge that the process is like the Southern Hemisphere Fans.
Thanks for the information about sublimation occurring in the Earth's atmosphere.
That defrosting dunes image and text you refer to hasn't been posted here, but feel free to add it and comment.
And it's much easier to land at lower altitudes because of the denser atmosphere.
Note also that those maps are based on estimates, there is no direct measurement of radiation levels at the surface. MSL will carry an instrument (RAD) to measure levels.
Some areas on Mars have weak fossil magnetic fields, these may also give extra protection from charged particles.