To interpret what these measurements mean, it is often necessary to know the temperature not just at the aircraft altitude -- where the chemical measurements are made -- but above and below the aircraft as well. The reason for this is that the vertical temperature profile provides meteorological context for the in situ measurements. For example, it is important to know whether the aircraft is in the troposphere (the lowest part of the atmosphere) or in the stratosphere (the next highest region). Ozone (O3) normally has much higher abundances in the stratosphere than the troposphere because it is produced there. Similarly, carbon monoxide (CO) has much higher abundances in the troposphere than in the stratosphere, because that's where it's produced. If high O3 and low CO are seen, one might conclude that the aircraft is in the stratosphere. However, this condition can occur occasionly in the troposphere, and the only way to know for sure what the real situation is is to measure where the thermal tropopause is located, as this separates the troposphere from the stratosphere. To do this this we need to measure an altitude temperature profile.
So how is the temperature profile of the atmosphere measured from an aircraft? There is really only one practicable, proven way to do this, and that is to use a microwave temperature profiler (MTP). Obviously the MTP must make a remote temperature measurement. It does this by detecting the naturally-occuring thermal emission of microwaves from oxygen molecules in the atmosphere. As is explained in the detailed version of this write-up, oxygen molecules satisfy several criteria which make such a measurement possible. When the MTP is scanned in frequency and elevation about the flight altitude, it measures the total emission from oxygen molecules along the viewing direction. The temperature profile is not measured directly however. The 20 or 30 measurements that the MTP makes in scanning from near-zenith to near-nadir, are converted into a temperature profile by performing a "retrieval" which takes into account where the aircraft is flying and the time of year. You might imagine that many different combinations of atmospheric conditions in the viewing direction might produce the same measurement, and you would be correct! The retrieval process, however, uses all of the measurements during a scan from zenith to nadir to figure out which is the most likely set of temperatures to produce the measurements, and this becomes the retrieved altitude temperature profile. In a nutshell, that is what an MTP does.
MTPs have a many more potential applications beyond their use as a research
instrument. They are useful for example in predicting the possibility of
clear air turbulence (CAT) and icing hazard potential for commercial aircraft,
and also improving their fuel efficiency. MTPs will also be able to detect
when unstart conditions will occur is a supersonic transport (SST) fleet
so that preventative measures can be taken. A key to making these and other
applications affordable is the development of monolithic microwave integrated
circuit (MMIC) technology, which will reduce the cost of manufacture by
about an order of magnitude.
Most people are familiar with in situ temperature measurements, where the thermometer is placed in or next to the thing whose temperature is to be determined. Often, however, this may not be possible: the medium may be so hot that the thermometer would either melt or loose calibration, or it may be so far away that it can't easily be reached. In these cases, remote sensing techniques must be used. Unlike in situ sensors, which rely on directly heating the thermometer (e.g., a mercury bulb or a thermistor), remote sensing techniques rely on detecting the energy radiated by the object or medium of interest, and then determining a temperature based upon the properties of the radiation. We are all familiar, for example, with the "heat" energy that we feel near a smoldering log. This energy, which is invisible to the human eye, is called infrared (IR) radiation and our skin has evolved to be able to sense it (for obvious reasons), just like our eyes have evolved to sense visible light (also for obvious reasons).
So
what is it about radiation that let's us measure temperature? Radiation,
or more properly electromagnetic radiation, is part of a broad energy spectrum
of naturally occuring thermal (and non-thermal) emissions which are carried
by particles called photons. Photons travel at the speed of light in a
vacuum, and their energy is characterized by either their wavelength or
their frequency. The most energetic photons have the shortest wavelengths
(highest frequencies), and include gamma rays and x-rays. In the "middle"
of the electromagnetic spectrum, at lower energy, are the ultraviolet (UV),
visible and infrared (IR) photons. Microwaves and long radio waves, the
least energetic of the photons, are at the longest wavelengths (lowest
frequencies). Now, without getting into the thermal physics of all this,
when an object is in thermodynamic equilibrium with its surroundings (that
is, when it emits and absorbs equal amounts of energy), the intensity of
its thermal emission at any frequency (or wavelength) depends on only one
thing -- it's temperaure! This remarkable fact, which physicists refer
to as the Planck Blackbody Distribution, is the basis for most remote temperature
measurements. Generally, remote temperature sensing is done in the infrared
at wavelengths between 0.7 and 20 microns. (see Infrared
Temperature Measurement Theory and Application for an introductory
discussion of IR remote sensing).
First, oxygen molecules radiate (and absorb) at a number of discrete frequencies between 50 and 70 GHz (microwaves with a wavelength of ~0.5 cm). These discrete frequencies, or spectral lines, are a consequence of rules of quantum mechanics which only allow oxygen molecules to have particular rotational energy states. Furthermore, since the oxygen molecules are in thermodynamic equilibrium with the local environment, this means that if we can measure the strength of the thermal emission from the oxygen molecules, then we can deduce the physical temperature of the molecules that produced this emission. Microwaves also have an advantage over infrared temperature sensing techniques in that they are only minimally affected by the presence of clouds. In addition, the receiver and detector technology is very mature.
Second,
the oxygen absorption is strong enough that the effective distance that
emission is "seen" from is of the order of a few kilometers, depending
on the frequency and altitude, as is shown in the figure, which illustrates
the absorption in units of Nepers/km for altitudes
of 0, 10, and 20 km. On the ground the oxygen absorption is a single broad
feature because individual oxygen emission lines have been blended together
by what is known as pressure broadening. At 10 km (~33,000 feet, the approximate
altitude jet liners fly) individual absorption features (spectral
lines) are beginning to be seen as pressure broadening of the emission
lines becomes less important, and at 20 km (the approximate altitude the
highest research aircraft fly) many individual spectral lines can be seen.
Because
any oxygen emission is absorbed in proportion to its distance from the
instrument detecting it (a MTP in our case), nearby emission is absorbed
little and the absorption increases exponentially with distance (r)
in the viewing direction, which in the figure is inclined to the direction
of flight. The integrated emission can be represented by a "weighting function"
(W(r)) which characterizes the weighted mean distance of the emission.
In the special case where the temperature lapses at a constant rate with
distance, it is easy to show that the brightness temperature measured by
the radiometer is exactly equal to the physical temperature at the e-folding
(Ra)distance for the absorption. More complicated situations
require more detailed treatment.
Third, oxygen molecules are a well-mixed component of the atmosphere at all heights, which is to say that the number of emitting molecules at any height depends only on the pressure altitude. Water vapor, for example, could not be used as a temperature surrogate because it's distribution (or mixing ratio) compared to its surroundings varies erratically. This characteristic is important because the strength of the signal emitted by the oxygen molecules (which we want to use to determine the temperature) depends not only on their temperature, but also on the number of emitting molecules (as measured by the pressure), and to a much lesser degree humidity. We must understand these dependencies to interpret our measurements. It is clear from the figure above that absorption decreases with altitude; the effect of temperature on absorption is opposite to pressure: lower temperatures increase absorption. These two effects somewhat offset each other, but pressure wins out and there is a net decrease of absorption with altitude.
The figure to the right shows how pressure and temperature vary with altitude
for a standard atmospheric model, which for the case shown represents average
conditions at mid-latitudes. Since pressure at any height is just the total
weight per unit area of all the air above, it decreases exponentially with
height (blue curve) and varies little from
the exponential shape shown. The behaviour of temperature (red
curve) is more complicated. It typically decreases with altitude
until the tropopause is reached. The rate of
temperature change with altitude (the lapse rate)
varies from about -10 K/km for dry air to about -5 K/km for moist air.
These large lapse rates are the result of convective mixing in the region
below the tropopause called the troposphere. This is where most weather
occurs. By contrast the region above the tropopause -- the stratosphere
-- is relatively benign as it is convectively stable. The temperature in
the stratosphere varies from being nearly constant (isothermal) at high
latitudes (the polar regions) to increasing slowly with altitude at low
latitudes (the tropics). The heat source in the stratosphere is the absorption
of ultraviolet radiation from the sun by ozone molecules.
An
MTP generally consists of two assemblies: a sensor unit (SU), which receives
and detects the signal, and a data unit (DU), which controls the SU and
records the data. In addition, on some platforms there may be a third element,
a real-time analysis computer (RAC), which analyzes the data to produce
temperature profiles and other data products in real time. The SU is shown
in the image to the right and the DU and RAC are shown in the image below.
The SU is connected to the DU with power, control, and data cables. In
addition the DU has interfaces to the aircraft navigation data bus and
the RAC, if one is present. Navigation data is needed so that information
such as altitude, pitch and roll are available for the MTP data analysis.
Aircraft altitude is needed to perform retrievals (which are altitude dependent),
while pitch and roll are needed for controlling the position of a stepper
motor which must drive a scanning mirror to predetermined elevation angles.
In
the SU image the scanning mirror is almost edge on and pointing slightly
upward and out of the page. The horn -- the equivalent of an antenna --
which receives the signal is perpendicular to the left side of the box
and faces the scanning mirror which is inclined at 45 degrees to the horn.
This mirror rotates about an axis through the horn which is nearly
normal to the flight direction (perpendicular to the side of the box with
JPL written on it) and allows viewing from near nadir (straight down) to
near zenith (straight up). At each viewing position a radio frequency signal
source, called a local oscillator (LO), is sequenced through two or more
frequencies and combined with the oxygen signal reflected off of the mirror
to produce a signal which is detected. A calibration target is the white
object behind the scanning mirror. The SU box dimensions are 14 cm W x
16 cm H x 24 cm D and it weighs ~5 kg. The DU and RAC are shown below in
a WB57F superpod. Their dimensions are 36 cm W x 10 cm H x 20 cm D and
25 cm W x 8 cm H x 35 cm D, respectively, and each unit weights ~5 kg.
Because each frequency has a different effective viewing distance, the MTP is able to "see" to different distances by changing frequency. In addition, because the viewing direction is also varied and because the atmospheric opacity is temperature and pressure dependent, different effective viewing distances are also achieved through scanning in elevation. For a two-frequency radiometer with 10 elevation angles, each 15-second observing cycle produces a set of 20 signals (called brightness temperatures), which are converted through a data analysis procedure called a linear retrieval algorithm to a profile of air temperature versus altitude, T(z).
Finally,
radiometric calibration is performed using the outside air temperature
(OAT) and a heated reference target to determine the instrument gain. However,
complete calibration of the system to include "window corrections" and
other effects, requires tedious analysis and comparison with radiosondes
near the aircraft flight path. This is probably the most important single
factor contributing to reliable calibration. For stable MTPs, such calibrations
appear to be reliable for many years. Such analysis is always performed
before MTP data are placed on mission archive computers. An example of
an altitude temperature profile (ATP) is shown to right in yellow. The
location of the tropopause is shown be the horizontal white dashed line;
the aircraft altitude is indicated by the short yellow horizontal line
at 35,000 feet (right scale), just below the tropopause. More information
on this and other MTP data products can be found here.
![]() |
DC8 on ramp in Shannon, Ireland
MTP is located in window just aft of forward starboard exit door Home field is at the Edwards, CA, Dryden Flight Research Center Go to this link to get more information on DC8 capabilities |
![]() |
Two ER2 aircraft flying over Golden Gate bridge in San Fransisco
MTP is located on right engine cheek. Home field is at the Edwards, CA, Dryden Flight Research Center Go to this link to get more information on ER2 capabilities |
![]() |
WB57F on ramp at Ellington Field, TX near Johnson
Space Center
MTP is located on right side of starboard wing superpod Home field is Ellington Field, TX |
| Platform | Dates | Acronym | Full Mission Name |
| WB57 | March-May 1998 | WAM | WB57 Aerosol Mission |
| DC8 | October-November, 1997 | SONEX | SASS Ozone and Nitrogen Oxide Experiment |
| ER2 | April - May 1997
June - July 1997 September 1997 |
POLARIS | Photochemistry of Ozone Loss in the Arctic Region In Summer |
| DC8 | April - May 1996 | SUCCESS | SUbsonic aircraft: Contrail & Cloud Effects Special Study |
| DC8 | December 1995 - February 1996 | TOTE/VOTE | Tropical Ozone Transport Experiment and
Vortex Ozone Transport Experiment |
| ER2 | May 1995
October - November 1995 January - February 1996 |
STRAT | Stratospheric Tracers of Atmospheric Transport |
Mixing Ratio By volume, the number of molecules of a particular specicies (e.g. water vapor) divided by the number of other molecules in a given volume. By mass, the mass of a particular species (e.g. water vapor) divided by the total mass of other molecules in a given volume.
Nepers/km A unit of absorption defined such that the reciprocal of this quantity is the e-folding distance for the signal attenuation; that is, the distance at which the signal is reduced by a factor of exp(-1), or 0.367 of the original signal strength. An absorption of 3 Nepers/km would reduce a signal of strength 1 unit to 0.05 units (or 5%) in one km.
Tropopause Because of convective
mixing in the lower atmosphere (i.e., the troposphere) temperature
decreases with increasing altitude because as rising air parcels enter
regions of lower pressure, they expand and cool. This continues until a
temperature inversion (that is, a warmer temperature) is encountered. At
this point, rising air parcels are heavier than the surrounding air and
sink back down. Normally this inversion occurs at the tropopause. Above
the tropopause (in the stratosphere) the air becomes warmer because
it is being heated by the absorption of ultraviolet sunlight by ozone.