Updated 3/19/02
Frequently Asked Questions
There are two major reasons why these observations can't be done from the ground:
Yes, the stars do vary in brightness all the time. In fact it is almost impossible to make a perfectly constant source of light. Fortunately, the stars we are most interested in are stars like our Sun. These are the most commonly seen dwarf stars and vary less than the change in brightness caused by an Earth-size planetary transit over the same time intervals as a transit duration.
Our Sun varies over many time scales: There are Maunder minimums, which do not occur for many centuries or longer and have caused "mini ice ages" even as recently as during the 17th century. There is an eleven year "solar cycle" of minimum and maximum activity. The largest short term variations are caused by "sun spots" that appear and fade, and rise and set as the Sun rotates with a period of four weeks.
Planetary transits have durations of a few hours to less than a day. The measured solar variability on this time scale is 1 part 100,000 (10 ppm) as compare to an Earth-size transit of 1 part in 12,000 (80 ppm). Even then most of the variability is in the UV, which is excluded from the measurements by the Kepler Mission .

There are three basic reasons why the HST could not be used to look for planets in the way described here:
Two recent research results have enabled the practicality of the Kepler Mission:
CCDs are at the heart of each "HandyCam" TV camera and special purpose CCDs are what we use for Kepler.
When light strikes a piece of silicon, it releases electrons that are free to move about the silicon material. These electrons form a charge or a current which is measured to determine the amount of light that has fallen on to the silicon.
In a CCD, the silicon region is divided electrically into small individual picture elements or pixels with about four hundred elements per cm in each direction, like a very finely divided sheet of graph paper. The free electrons are kept from moving around by permanent channel stops (the vertical lines in the figure) and externally applied voltages (the horizontal lines in the figure). Each pixel can then be thought of as an individual bucket or well that collects electrons.
As shown in the animation, first the CCD is exposed to light from a telescope or camera lens. Overtime this produces an image made up of electrons in the CCD.
To readout an image that has been captured with the CCD requires shifting the information out of the pixels. First, the columns of pixels are all shifted down one row. The bottom row of pixels is shifted into a readout register. Each pixel in the readout register is shifted out to an amplifier and the number of electrons in each pixel are recorded. This produces a series of 1's and 0's that represent the image. This is repeated over and over until all the pixels have been read. The stream of 1's and 0's is then digitally processed to reproduce the image that is later displayed.
In the Kepler Mission the 1's and 0's are recorded onboard the spacecraft and sent to the ground, where the data are processed to look for changes in the brightness of each star that may be caused by a planetary transit.
A representation of the scientific performance versus project cost is shown in the figure. A well conceived project is at A with maximum possible science per dollar available. Many times, those who fund a program perceive the project to be at B, where costs can be cut without much loss in science; well the science team tries to believe that they are at C, where more science can be achieved at little extra cost. Good clever scientists and engineers might be able to get to point D, but this is unusual. Project managers worth their weight in gold are those who can push toward E, keeping the performance, but saving on cost Any project headed from A to B, A to C or A to F is doomed to be canceled or should be canceled.
For the Kepler Mission to work, a 100,000 main-sequence stars must be monitored to a differential photometric precision of 1:50,000 every 6.5 hours. Substantially fewer stars and the results may turn out to be ambiguous. The necessary precision requires recording ten billion photons from each star every 6.5 hours. Thus, a smaller photometer would mean either fewer stars at the required precision or poorer precision for most of the stars and thereby the inability to detect Earth-size planets. Also, the photometer would need to be much smaller before other costs, such as the launch vehicle, would begin to drop significantly.
Our project manager has worked hard at both increasing the performance by increasing the downlink data rate to permit monitoring 100,000 stars (originally we planned to monitored only 5000 stars) and in reducing the cost by changing the orbit to an Earth-trailing heliocentric orbit and thereby eliminating an expensive propulsion stage needed to get to an L2 halo orbit. This also allowed us to use a smaller and less costly launch vehicle. In essence, we have already pushed the cost-performance curve in both the D and E directions.
There are three photometry mission that are already under development. However, they are considerably less capable than the Kepler Mission , since their primary science mission is to measure the properties of stars. These mission are COROT, MONS and MOST. COROT has 1/10 the collecting area for photons, 1/20th the field of view of the sky and stares at a given star field for 1/10 the amount of time that the Kepler Mission stares. MONS and MOST are even smaller missions and less capable.
Another mission proposed to ESA, Eddington, is somewhat closer to the Kepler Mission in capability. It has almost the same collecting area and hence should achieve similar noise performance for the same star brightness. However, it only has a field of view of 1/15 of the Kepler Mission and only views the field for a maximum of 3 years rather the Kepler's 4 years, hence its effective SNR is about sqrt(3/4) of Kepler for an equivalent transit of a similar stellar brightness.
Obtaining astrophysical information about each star is a natural byproduct of detecting planetary transits. The following are some of the potential uses for these data:
Phenomena
Stellar rotation rates
p-mode oscillations
.Characteristics of solar-type stars
Frequency of Maunder minimum
Stellar activity
.Cataclysmic variables
Eclipsing binaries
Active Galactic Nuclei variability
Information Obtained
Variation in rates with stellar type
Window on stellar interior:
mass, age, metallicity of starsDetermine what is a "normal" star
Earth climate implications
Star spot cycles, white light flaring,
PaleoclimatologyPre-outburst activity, mass transfer
Detection of high-mass ratio binaries
"Engine" size in BL Lac, quasars and blazars
The Kepler Mission contributes in several ways to both the Space Interferometry Mission (SIM) and the Terrestrial Planet Finder (TPF) mission:

Curator: David Koch