Canadian Arrow Announces Test Launch Plans

Image credit: Canadian Arrow
Canadian Arrow is pleased to announce that it will begin unmanned test flights of its rocket this summer. The flights, taking place over a period of four months beginning in August, will test the Arrow?s launch pad abort system and escape systems. This testing will be essential before any manned launches are attempted.

The Arrow is currently completing arrangements for the tests at an Ontario location, which will be announced at a future date. The tests will include:

? A launch pad abort test, including testing of the powerful solid rockets that pull the crew cabin to safety in the event of problems while the rocket is on the pad.
? Separation of the nose cone from the crew cabin.
? Deployment of parachutes for safe recovery of the nose cone and crew cabin.
? Testing of aerodynamics to ensure the rocket is able to reach the correct altitude and does not display any flight characteristics that are not normal to flight.
? A mach 1 abort and high altitude abort (application for permission to fly currently being processed)

Specifications of escape system:
? Eight 1,200 lb thrust solid rocket engines that burn for 5 seconds, mounted in a 22-ft tall nose cone
? Two main parachutes 64 ft in diameter
? Onboard computer to record data including acceleration, vibration, pitch, yaw and roll of the rocket.
? Onboard video camera aimed out the same window as the astronauts will use. Video will be available to the media after the flight.
? Vehicle will weigh 2,500lbs at liftoff.
? Crew cabin (space capsule) designed to carry three astronauts 65 inches in diameter and 6 ft tall.

The Canadian Arrow will also fly its first XPOD experiment, produced by students at the Canadian Arrow Science Club at John Dearness School in London. The flight will test the durability of the XPOD. Canadian Arrow is a London-built rocket, competing for the $10 million (US) X PRIZE, which will go to the first team that can launch a passenger space vehicle 100 kilometres into space, land safely and repeat the feat within two weeks.

Original Source: Canadian Arrow News Release

Stardust Surprised Scientists

Image credit: NASA/JPL

When NASA’s Stardust spacecraft swept past Comet Wild-2, it captured material from the comet’s tail and revealed incredible details about the surface of the fast moving object. The few images that Stardust was able to take also provided some surprises. Scientists anticipated that that comet would be a dusty snowball, with very few surface features, but Stardust found impact craters, barn-sized boulders, and tall cliffs. This indicates that the comet isn’t the loose collection of material that scientists theorized, since it’s obviously withstood quite a beating.

On Jan. 2nd, 2004, NASA’s Stardust spacecraft approached Comet Wild 2 and flew into a storm. Flurries of comet dust pelted the craft. At least half a dozen grains moving faster than bullets penetrated Stardust’s outermost defenses. The craft’s 16 rocket engines struggled to maintain course while a collector, about the size of a tennis racquet, caught some of the dust for return to Earth two years hence.

All that was expected.

Then came the surprise. It happened when Stardust passed by the core of the comet, only 236 km distant, and photographed it using a navigation camera. The images were intended primarily to keep the spacecraft on course. They also revealed a worldlet of startling beauty.

Right: The nucleus of Comet Wild 2 photographed by Stardust with approximately 20 meter resolution. Click on the image to see a much larger version.

At the heart of every comet lies a “dirty snowball,” a compact nucleus of dust and ice that the sun vaporizes, little by little, to form the comet’s spectacular tail. These nuclei are hard to see. For one thing, most are blacker than charcoal; they reflect precious little sunlight for cameras. Plus they’re hidden deep inside a cloud of vaporizing gas and dust, called “the coma.” Stardust’s plunge into Wild 2’s coma allowed it to view the nucleus at close range.

Previous flybys of Comet Halley by the European Giotto probe and Comet Borrelly by NASA?s Deep Space 1 revealed lumpy cores without much interesting terrain–as expected. These comets have been sun-warmed for many thousands of years. Solar heating has melted away their sharpest features.

Comet Wild 2, however, looks different. “We were amazed by the feature-rich surface of the comet,” says Donald Brownlee of the University of Washington, the mission’s principal investigator. “It is highly complex. There are barn-sized boulders, 100-meter high cliffs, and some weird terrain unlike anything we’ve ever seen before. There are also some circular features,” he adds, “that look like impact craters as large as 1 km across.”

“The high cliffs tell us that the crust of the comet is reasonably strong,” notes Brownlee. It’s probably a mixture of fine-grained rocky material held together by frozen water, carbon monoxide and methanol. Certainly a lander could touch down there, or an astronaut could walk across the surface without worrying too much about the ground collapsing.

An astronaut standing on Comet Wild 2 would see a truly fantastic landscape, speculates Brownlee. ?I imagine them inside one of the craters, surrounded by deep cliffs.” Icy spires, as tall as a person, might rise out of the crater floor. “These would be be the comet-equivalent of ‘snow spikes’ on Earth–those little jagged ridges that form when snow is exposed to sunlight and melts.”

Getting out of the crater would be easy. “Just jump,” says Brownlee, “but not too hard.” The comet?s gravity is only 0.0001-g, so “you could easily leap into orbit.”

Some of the photos from Stardust reveal gaseous jets. “The jets come from active regions on the comet’s surface, fissures or vents probably, where the ice is vaporizing and rushing into space,” Brownlee says. This is how mass is transferred from the comet’s nucleus to its tail.

Viewed from the surface, the jets would be nearly transparent. But an astronaut could spot them by looking for “dust entrained with the gas. Dust grains glinting in the sunlight would look like tracer bullets shooting out of the ground.”

A careful explorer could survey the entire 5-km nucleus in only a few hours, leaping high above the surface, dodging the occasional jet. “What an experience that would be,” he says.

There are billions of comets in the solar system. “We’ve gotten a close-up look at only three,” says Brownlee. And one of the three, Comet Halley, presented its night side to the cameras. So it’s too soon to say whether Comet Wild 2, among comets, is truly unusual.

Unlike comets Halley and Borrelly, notes Brownlee, “Wild 2 is a very recent arrival to the inner solar system.” For billions of years it orbited in the cold deep space beyond Jupiter, until 1974 when it was nudged by Jupiter’s gravity into a sun-approaching orbit. Since then the comet has passed by the Sun only five times; solar heating is only beginning to mold its surface.

And, according to Brownlee, that might be the key to the comet’s appearance. “Wild 2’s surface is a mixture of young and old that we haven’t see before,” he explains. Young features include possible sinkholes collapsing as the terrain is warmed. Impact craters and their ejecta, on the other hand, are old scars from time spent in the outer solar system.

The old parts of Wild 2 are what make the comet an attractive target for the Stardust probe, which captured a thousand or more grains of comet dust during the flyby. Such material, little altered since the formation of the solar system, could tell us a great deal about our origins.

The craft’s payload will return to Earth in 2006 for analysis by scientists. If a single picture from the navigation camera can surprise researchers, just imagine what’s in store when they get their hands on a thousand pieces of the comet itself.

Original Source: Science@NASA

SMART-1 Gets Out of the Radiation Belts

Image credit: ESA

The European Space Agency’s SMART-1 spacecraft has completed its 176th orbit around the Earth, finally reaching the outer limits of our planet’s Van Allen radiation belts. After weeks in the intense radiation, it looks like everything on SMART-1 is functioning normally. The spacecraft has fired its ion thruster for a total of 1,500 hours and only consumed 24 kg of Xenon fuel. SMART-1 is taking the slow road to the Moon, where it will map the surface and search for deposits of ice.

The spacecraft is now in its 176th orbit, in good status and with all functions performing nominally. The first mission target, namely to exit the most dangerous part of the radiation belts, has been achieved! The pericentre altitude (the closest distance of the spacecraft from the centre of the Earth) will reach the prelaunch target of 20 000 km on 7 January 2004.

Between 23 December 2003 and 2 January 2004, the thruster fired continuously for a record duration of more than 240 hours. This is likely to remain the record for some time because later this week SMART-1 will change from a continuous thrust strategy to a more orbitally efficient thrust arcing.

The total cumulated thrust so far of more than 1500 hours, consuming 24 kg of Xenon, has provided a velocity increment of about 1070 ms-1 (equivalent to 3850 km per hour). The electric propulsion engine’s performance, periodically monitored by means of the telemetry data transmitted by the spacecraft and by radio-tracking by the ground stations, continues to show a small over performance in thrust: varying from 1.1% to 1.5% over the last week.

The degradation of the electrical power produced by the solar arrays has now ceased. The power available has remained virtually constant since November 2003.

The communication, data handling, on-board software and thermal subsystems have been performing well in this period.

Original Source: ESA News Release

One Day to Go for Beagle 2

This time of year, I usually wind things down at Universe Today since the various news sources are all on holiday and there isn’t much to report. This year; however, it’s an entirely different story. The British-built Beagle 2 lander will be touching down on Mars on December 25. Stardust reaches Comet Wild 2 on January 2, and the Mars Exploration Rover arrives on January 3. Things couldn’t be busier.

So, first up… Beagle 2 and Mars Express. The lander is expected to arrive at 0254 UTC on December 25 (9:54 pm EST December 24). We won’t know if Beagle 2 arrived safely for another four hours or so, when Mars Express enters orbit – data won’t arrive back on Earth until 0700 UTC (2:00am EST). Keep your fingers crossed.

The European Space Agency has said they’ll be broadcasting information about the landing live on television, but I haven’t been able to find a link on the web for it (if you know of one, let me know). You can visit their special coverage of the landing and Mars Express arrival here. Or go straight to the Beagle 2 website, where they’ll just be focused on the lander. As I find cool stuff on the web, I’ll let you know.

And make sure you come visit the Universe Today forum and share your thoughts and ideas about the missions with the rest of our community.

Have a happy and safe holiday. See you on Mars!

Fraser Cain
Publisher
Universe Today

Beagle 2 Separates from Mars Express

Image credit: ESA

The European Space Agency’s Mars Express spacecraft successfully released the British-built Beagle 2 lander this morning, completing a major milestone on its trip to Mars. Mars Express fired a pyrotechnic device which slowly released a spring and separated the two spacecraft. Since Beagle 2 has no propulsion system, controllers have no way of fine-tuning the lander’s flight path. If everything goes as planned, Beagle 2 will enter the planet’s atmosphere on December 25.

This morning, ESA’s Mars Express flawlessly released the Beagle 2 lander that it has been carrying since its launch on 2 June this year. Beagle 2 is now on its journey towards the surface of Mars, where it is expected to land early in the morning of 25 December. Mars Express, Europe’s first mission to Mars, has passed another challenging milestone on its way towards its final destination.

At 9:31 CET, the crucial sequence started to separate the Beagle 2 lander from Mars Express. As data from Mars Express confirm, the pyrotechnic device was fired to slowly release a loaded spring, which gently pushed Beagle 2 away from the mother spacecraft. An image from the on-board visual monitoring camera (VMC) showing the lander drifting away is expected to be available later today.

Since the Beagle 2 lander has no propulsion system of its own, it had to be put on the correct course for its descent before it was released. For this reason, on 16 December, the trajectory of the whole Mars Express spacecraft had to be adjusted to ensure that Beagle 2 would be on course to enter the atmosphere of Mars. This manoeuvre, called ‘retargeting’, was critical: if the entry angle is too steep, the lander could overheat and burn up in the atmosphere; if the angle is too shallow, the lander might skim like a pebble on the surface of a lake and miss its target.

This fine targeting and today’s release were crucial manoeuvres for which ESA’s Ground Control Team at ESOC (European Space Operations Centre) had trained over the past several months. The next major milestone for Mars Express will be the manoeuvre to enter into orbit around Mars. This will happen at 2:52 CET on Christmas morning, when Beagle 2 is expected to land on the surface of Mars.

“Good teamwork by everybody – ESA, industry and the Beagle 2 team – has got one more critical step accomplished. Mars, here comes Europe!” said David Southwood, ESA Director of Science.

Original Source: ESA News Release

SMART-1 at Full Speed

Image credit: ESA

The European Space Agency’s SMART-1 spacecraft is continuing to function well on its long roundabout mission to the Moon. The spacecraft recently completed its 139th orbit and everything seems to be functioning properly, despite the recent solar storms that damaged a few other satellites. It’s running its solar-powered ion drive full time now, and incrementally raising its distance with each orbit around the Earth. SMART-1 will reach its final orbit around the Moon in March 2005.

The spacecraft is now in its 139th orbit, in good operational status and with all functions performing nominally. As previously, the spacecraft was operated in electric propulsion mode almost continuously.

This week we had no flame-outs, probably due to the adopted strategy not to thrust when the orbital altitude is less than 10 000 km. The procedure to automatically re-start the engine after a flame-out will be uploaded to the on-board software this week. Once this is in place, the thrust phase will no longer be interrupted.

The total cumulated thrust time is now more than 946 hours and SMART-1 has consumed almost 15 kg of Xenon. Even with such a low fuel consumption the electric propulsion engine has so far provided a velocity increment of about 665 ms-1 (equivalent to about 2400 km per hour). The electric propulsion engine’s performance, periodically monitored from telemetry data and by ground stations tracking, continues to show a small over performance in thrust, varying from 1.1% to 1.5% over the last week.

The newly adopted strategy to thrust in a direction perpendicular to the position vector in the orbital plane has produced a large perigee increase in the last week of more than 1200 kilometres (see orbital elements and orbit picture).

The degradation of the electrical power produced by the solar arrays is now slowing down considerably. As a matter of fact the available power has remained more or less constant in the last 15 days. This means that the degradation by radiation has matched the increase of solar irradiance due to the nearing of the Earth’s perihelion, so that the net effect is zero. This is explained by the fact that no direct proton radiation from solar activity was experienced and the fact that the spacecraft now stays outside of the radiation belts for a considerable part of its orbit.

The communication, data handling and on-board software subsystems have been performing very well in the last week.

The thermal subsystem continues to perform well and all the temperatures are as expected. The temperature of the optical head on star tracker #1 is now lower than before. This is due to the changed thrust attitude which reduces the exposure to the Sun of the ?Z side of the spacecraft. Other attitudes are being considered in order to test the dependence of the star tracker’s temperature upon the spacecraft’s attitude.

Orbital/Trajectory information
The SMART-1 orbit is continuously modified by the effects of the electric propulsion low thrust. The osculating orbital elements are periodically computed by the ESOC specialists. These elements define the so called osculating orbit which would be travelled by the spacecraft if at that instant all perturbations, including EP thrust, would cease. So it is an image of the situation at that epoch. In reality the path travelled by the spacecraft is a continuous spiral leading from one orbit to another. The most recent osculating elements are as follows:

From the start, the electric propulsion system has managed to increase the semi-major axis of the orbit by 6750 km, increasing the perigee altitude from the original 656 km to 7012 km and the orbital period by more than four and a half hours, from the initial 10 hours 41 minutes to the present 15 hours 22 minutes.

Original Source: ESA News Release

Pluto Mission Will Study Jupiter Too

Image credit: SWRI

Although the main goal of the NASA’s New Horizons mission will be to send a spacecraft to Pluto, the mission designers figure they can examine Jupiter on the way out as well – and get a valuable gravity boost that would shave years off the mission. If all goes as planned, New Horizons would launch in 2006, and pass Jupiter in early 2007 (probably three times closer than Cassini did in 2000); it will reach the Pluto-Charon system in 2015. After Pluto, New Horizons would then be re-targeted to fly past a Kuiper Belt Object.

The main goal of NASA’s New Horizons mission may be to explore Pluto-Charon and the Kuiper belt beginning in 2015, but first the mission plans to fly by the solar system’s largest planet, Jupiter, during February-March 2007. The Jupiter flyby would be used by New Horizons to provide a gravitational assist that shaves years off the trip time to Pluto-Charon and the Kuiper belt.

During the flyby, plans call for New Horizons to use its instrument payload, consisting of cameras, spectrometers, radiometers, and space plasma and dust sensors, to make a variety of scientific observations. Toward that end, the New Horizons team has formally kicked off its planning of the Jupiter flyby science observations. Southwest Research Institute? (SwRI?) and the Johns Hopkins University Applied Physics Laboratory (APL) lead the mission. Major partners include Ball Aerospace, Lockheed-Martin, Boeing, NASA Goddard Space Flight Center and the California Institute of Technology Jet Propulsion Laboratory.

“Every spacecraft must check out its instruments and pointing capabilities in flight prior to reaching its target,” says mission project scientist Dr. Hal Weaver of the Johns Hopkins University Applied Physics Laboratory. “By virtue of the gravity assist maneuver at Jupiter, New Horizons has a unique opportunity to do its check out on a very worthy and exciting scientific target.”

“New Horizons presents NASA’s next opportunity to study the complex and fascinating Jupiter system,” says Dr. Alan Stern, principal investigator of the New Horizons mission and director of the SwRI Space Studies Department. “To accomplish its gravity-assist maneuver on the way to Pluto-Charon, our spacecraft will venture at least three times closer to Jupiter than the Cassini spacecraft did in late 2000 when it used Jupiter for a gravity assist on the way to Saturn.

“Astronomically speaking, we will fly just outside of the edge of Jupiter’s large, planet-sized Galilean moon, Callisto.” From its closer range, New Horizons will perform a number of Jupiter system studies not possible from Cassini’s greater flyby distance.

Science planning is going forward to ready the mission for its planned 2006 launch, at the same time that required environmental and safety reviews are also being done. Through the summer of 2004, the New Horizons science team will prioritize its Jupiter science activities from objectives provided by team members as well as interested scientists from around the world. To accomplish this objective, Stern has appointed mission co-investigator and imaging team lead Dr. Jeff Moore of the NASA Ames Research Center to lead the New Horizons Jupiter Encounter Sequencing Team (JEST).

“New Horizons will be the next mission to Jupiter, and it is carrying a sophisticated instrument complement,” says Moore. “We intend to cull and then schedule the most critical needs for scientific observations of Jupiter, its satellites, its magnetosphere and its rings.

“Following that,” Moore continued, “the mission team will design and implement a five-month-long sequence of observations of the Jupiter system to be made from late 2006 through early 2007 as the spacecraft approaches and then recedes from Jupiter.”

“Exploring the Jupiter system is a coveted scientific bonus for New Horizons,” adds Weaver. “It also provides us with a valuable opportunity to check out the instrument payload and many of the flyby procedures we will later use at Pluto-Charon.”

New Horizons is proceeding toward a January 2006 launch, with a planned arrival at Pluto and its moon, Charon, in the summer of 2015. The 465-kilogram (1,025-pound) spacecraft will characterize the global geology and geomorphology of Pluto and Charon, map the surface compositions and temperatures of these worlds, and study Pluto’s atmospheric composition and structure. It will then visit one or more of the icy, primordial bodies in the Kuiper belt where it will make similar investigations.

In July 2002, the National Research Council’s Decadal Survey for Planetary Science ranked the reconnaissance of Pluto-Charon and the Kuiper belt as its highest priority for a new start mission in planetary science, citing the fundamental scientific importance of these bodies to advancing understanding of our solar system.

Original Source: SWRI News Release

NASA Tests a New Ion Engine

Image credit: NASA

NASA has tested a new high-power ion engine which could give future spacecraft significantly more thrust to accomplish exploration of the solar system. The High Power Electric Propulsion (HiPEP) ion engine should eventually be 10 times as powerful as NASA’s Deep Space 1 ion engine which was tested a few years ago. An engine like this will probably power the JIMO probe allowing it to go into and out of orbit around several of Jupiter’s moons and map them in great detail.

NASA’s Project Prometheus recently reached an important milestone with the first successful test of an engine that could lead to revolutionary propulsion capabilities for space exploration missions throughout the solar system and beyond.

The test involved a High Power Electric Propulsion (HiPEP) ion engine. The event marked the first in a series of performance tests to demonstrate new high-velocity and high-power thrust needed for use in nuclear electric propulsion (NEP) applications.

“The initial test went extremely well,” said Dr. John Foster, the primary investigator of the HiPEP ion engine at NASA’s Glenn Research Center (GRC), Cleveland. “The test involved the largest microwave ion thruster ever built. The use of microwaves for ionization would enable very long-life thrusters for probing the universe,” he said.

The test was conducted in a vacuum chamber at GRC. The HiPEP ion engine was operated at power levels up to 12 kilowatts and over an equivalent range of exhaust velocities from 60,000 to 80,000 meters per second. The thruster is being designed to provide seven-to-ten-year lifetimes at high fuel efficiencies of more than 6,000-seconds specific impulse; a measure of how much thrust is generated per pound of fuel. This is a contrast to Space Shuttle main engines, which have a specific impulse of 460 seconds.

The HiPEP thruster operates by ionizing xenon gas with microwaves. At the rear of the engine is a pair of rectangular metal grids that are charged with 6,000 volts of electric potential. The force of this electric field exerts a strong electrostatic pull on the xenon ions, accelerating them and producing the thrust that propels the spacecraft. The rectangular shape, a departure from the cylindrical ion thrusters used before, was designed to allow for an increase in engine power and performance by means of stretching the engine. The use of microwaves should provide much longer life and ion-production capability compared to current state-of-the-art technologies.

This new class of NEP thrusters will offer substantial performance advantages over the ion engine flown on Deep Space 1 in 1999. Overall improvements include up to a factor of 10 or more in power; a factor of two to three in fuel efficiency; a factor of four to five in grid voltage; a factor of five to eight in thruster lifetime; and a 30 percent improvement in overall thruster efficiency. GRC engineers will continue testing and development of this particular thruster model, culminating in performance tests at full power levels of 25 kilowatts.

“This test represents a huge leap in demonstrating the potential for advanced ion technologies, which could propel flagship space exploration missions throughout the solar system and beyond,” said Alan Newhouse, Director, Project Prometheus. “We commend the work of Glenn and the other NASA Centers supporting this ambitious program.”

HiPEP is one of several candidate propulsion technologies under study by Project Prometheus for possible use on the first proposed flight mission, the Jupiter Icy Moons Orbiter (JIMO). Powered by a small nuclear reactor, electric thrusters would propel the JIMO spacecraft as it conducts close-range observations of Jupiter’s three icy moons, Ganymede, Callisto and Europa. The three moons could contain water, and where there is water, there is the possibility of life.

Development of the HiPEP ion engine is being carried out by a team of engineers from GRC; Aerojet, Redmond, Wash.; Boeing Electron Dynamic Devices, Torrance, Calif.; Ohio Aerospace Institute, Cleveland; University of Michigan, Ann Arbor, Mich.; Colorado State University, Fort Collins, Colo.; and the University of Wisconsin, Madison, Wis.

A print quality photograph of the HiPEP ion engine is at:
http://www.grc.nasa.gov/WWW/PAO/pressrel/2003/03-079addm.html

For information about NASA on the Internet, visit:
http://www.nasa.gov

For more information about NASA’s Glenn Research Center, visit:
http://www.grc.nasa.gov

For more information about Project Prometheus on the Internet, visit:
http://spacescience.nasa.gov/missions/prometheus.htm

Information about JIMO is available on the Internet at:
http://spacescience.nasa.gov/missions/JIMO.pdf

Original Source: NASA News Release

Gravity Probe B Launch Delayed

Image credit: NASA

NASA has decided to push back the launch of its mission to test Einstein’s theory of general relativity, Gravity Probe B, until December 6. During recent tests, engineers noticed electronic noise coming from the sensor attached to one of the spacecraft’s gyros, so they’ve extended the launch date to find time to fix it. Once it does launch, Gravity Probe B will detect any distortions on its four spinning gyroscopes to detect the Earth’s distortion of spacetime around it – as predicted by Einstein.

After a review of test data, a decision has been made to reschedule the launch of Gravity Probe B (GP-B). The launch had been scheduled for Dec. 6 from Vandenberg Air Force Base in California.

Data obtained during spacecraft prelaunch testing shows electronic noise on an output channel associated with the No. 1 experiment gyro. This could compromise the quality of data received from it. The problem has been isolated to a component in the spacecraft?s experiment control unit (ECU). While there is a second available output channel for this gyro, a postponement of the launch will allow time for a repair. This precaution will restore full redundancy to the experiment and provide the greatest chance for success over the planned 16-month life of the mission.

At Space Launch Complex 2, the rocket has successfully completed the scheduled prelaunch preparations up to this time, and there are no issues or concerns with the Delta II. The current plans are for it to remain at the pad enclosed within the gantry-like mobile service tower until the spacecraft arrives.

The length of the postponement will not be known for about a week until a course of action has been developed to address the GP-B problem.

Original Source: NASA News Release

ESA Cancels Eddington

Image credit: ESA

The European Space Agency announced this week that it has canceled Eddington, a space-based observatory designed to search for extrasolar planets. They’re also going to be scaling back the BepiColombo mission to Mercury by removing the lander that was supposed to accompany the spacecraft. The agency blamed the cuts on budget overruns with other missions, such as Rosetta. One new mission was announced, however. The LISA Pathfinder will serve as a prototype to help search for gravity waves.

Today, at its 105th meeting, ESA’s Science Programme Committee (SPC) has made important decisions concerning the Cosmic Vision programme. Due to the current financial exigencies and an outlook with no budget increase or other relief, the SPC was forced to cancel the Eddington mission and rescope the BepiColombo mission.

Eddington had two aims, both remarkable and very pertinent to front-line astronomical interests. The first aim was to look for Earth-like planets outside our solar system – one of the key goals in the search to understand how life came to be, how we came to live where we do in the universe and whether there are other potential life supporting environments ‘out there’. At the same time it was going to follow on the path blazed by the ESA-NASA mission SOHO had taken with the Sun of using astroseismology to look ‘inside’ stars. In the longer term, the loss of this one mission will not stop us pursuing the grand quests for which it is a step.

The loss of the BepiColombo lander is also scientifically hard to take. ESA, in conjunction with the Japanese space agency, JAXA, will still put two orbiters around Mercury but the ?ground truth? provided by the lander is a big loss. However, to land on a planet so near the Sun is no small matter and was a bridge too far in present circumstances, and this chance for Europe to be first has probably been lost.

The origins of the problems were recognized at the ESA Council, held in June 2003. Several sudden demands on finance occurred in the spring, the most obvious and public being the unforeseen Ariane 5 grounding in January. A loan of 100 million Euro was temporarily granted, that must be paid back out of present resources by the end of 2006.

ESA’s SPC were therefore caught in a vice. Immediate mission starts had to be severely limited and the overall envelope of the programme kept down.

By making today’s decision, the SPC has brought down the scope of the Cosmic Vision programme to a level that necessarily reflects the financial conditions rather than the ambitions of the scientific community.

A long and painful discussion during the SPC meeting resulted in the conclusion that only one new mission can be started at this time, namely LISA Pathfinder. The mission is the technical precursor to the world?s first gravitational wave astronomical observatory, LISA. The LISA mission itself (to be made in cooperation with the United States) is scheduled for launch in 2012.

ESA’s Cosmic Vision, set to last until 2012, is a living programme. It has to be able to constantly adapt to to the available funding as well as respond to the expectations of the scientific community, to technological developments. Within these boundaries, the decisions made by the SPC try to maximize the outcome of Cosmic Vision across disciplines, keeping it at the same time challenging and affordable. Nonetheless, there are many European scientists with ambitions that exceed the programme?s ability to respond.

Original Source: ESA News Release