Radar
Sees The Weather
From the 1981 KOY Almanac By Ed Phillips, and when Ed changed
employment, later to be published by KTAR. This was page 40. We have this
AVQ-10 Radar
The word radar means Radio Detection And Ranging. Simply put, a radar
is a device used to detect distant objects that reflect radio energy.
Since only objects that reflect energy show up on the radar screen, they
are called "echoes."
In the case of a weather radar, the energy is reflected because of
precipitation, not clouds, aircraft or dust. This feature enables the user
to 'see' within the clouds and find out if they are producing rain or
snow. The rain and snow echoes are displayed on a screen much like a T.V.
picture. From the location on the screen, the operator can determine the
direction and distance the rain is away from the radar unit.
The KOY Weather Station is equipped with weather radar. An RCA AVQ-10
Aircraft Radar has been modified for stationary operation. With our radar,
the strongest storms can be seen 150 nautical miles away. The distance you
can see rain is of course limited by mountains and buildings because the
radar signal travels in a straight line. Our radar set also has a fifty
mile range. We use it most often because it gives good coverage to all of
the Salt River Valley. A 20 mile range is also available to use when
storms are in close range. We operate our radar any time rain is
threatening the valley. KOY is the only broadcasting station in the valley
that has weather radar. Radar updates are given every half hour during
morning and afternoon drive times when there is rain around. If severe
weather threatens, you can count on us to have the storms pinpointed and
keep you abreast of the latest weather developments.
40
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(These 3 photos
are from the 1980 version of the KOY Ed Phillips Almanac they are
different than those in the 1981 version and special as
it shows the radar screen in 2 of them! see more at http://www.smecc.org/6BBH_-_KDYM_-_KFCB_-_KOY_-_history.htm
)
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Dean Reed and Ed Sharpe
C
BAND AIRBORNE SEARCH.
Radar type: AVQ-10. Freq: 5.4 GHz. Pwr output: 16KW. Indicator: 5" PPI.
Magnetron type: 6521. Rep rate: 2 us at 4000 PPS. Pwr input: 115V, 400 Hz. Mfr:
RCA.
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WEATHER RADAR AVQ-10
Complete AVQ-10 system, showing
receiver-transmitter unit, antenna, control panel, accessory unit and
two indicators.
WHAT IT IS . . .
The AVQ-10 is a lightweight airborne radar, designed specifically to
meet the exacting requirements of airline and executive transport
operators.
WHAT IT DOES. . . The AVQ-10 can "see' storms and show
nonturbulent paths through or around them. This feature of highly accurate
"in flight" weather reconnaissance permits pilots to navigate
between storm cores and around turbulent areas, ,enabling operators to
maintain flight schedules and provide smoother rides for their passengers.
The AVQ-10 also provides for terrain mapping by adequately identifying
land and water masses and detecting mountains.
means
ECONOMY OF OPERATION
Installation of AVQ-10 will greatly improve operational economy by
permitting closer adherence to schedules and minimizing long detours or
flight cancellations.
PASSENGER COMFORT
There is nothing more disturbing to an airline customer than passage
through turbulent areas. These areas, which sometimes cause extremely
rough riding, not only induce air sickness, but may inconvenience
passengers to the extent of possibly discouraging future air travel. The
AVQ-10 will enable planes to avoid most turbulent areas, thus providing a
smoother ride and, subsequently, greater peace of mind for passengers.
ARRIVAL TIME DEPENDABILITY
By avoiding turnbacks and extensive detours, planes will be able to
arrive more frequently on schedule. This improvement of arrivaltime
dependability will gain passenger confidence.
REDUCTION OF PILOT FATIGUE
Pilots have long been plagued by the uncertainty and unpredictability
of weather conditions while in flight. The inadequate storm warning
facilities of any meteorological system and the constantly changing
turbul,ent conditions aloft require untiring visual vigilance on the part
of these pilots. This constant state of tension can result in excessive
fatigue. The use of the AVQ-I0, especially on extended flights under IFR
conditions, will reduce the strain on pilot reflexes by providing
better-than-sight interpretation of weather conditions and provides these
features
ISO ECHO CONTOUR FEATURE
Accurate interpretation of scope information can be acquired by pilots
with a minimum amount of training. Analyzing the degree of turbulence
displayed in a PPI picture has been simplified by the use of ISO Echo
Contour principles. Generally, the brighter the intensity of display the
more dense the rainfall. The PPI, however, can only display a certain
degree of intensity; consequently, progressively heavier rainfall areas
will appear uniform on the display, which is not a true picture. The ISO
Echo Contour circuit provides for a black picture to appear on the PPI
when the signal return intensity reaches a preset level. The black areas
on the scope then represent the storm cores, the areas of greatest
moisture density. By avoiding these blacked out areas, the pilot can avoid
the areas of greatest turbulence.
LIGHTWEIGHT CONSTRUCTION
Weight factors were given prime consideration in the design of the
AVQ-I0. As a result, substantial weight reductions were made without any
loss of quality, operating capability or penetration
A complete AVQ-10 system, including all units (less shock mounts),
weighs less than 125 pounds.
BRIGHT DISPLAY INDICATOR
The AVQ-10 has been constructed so that an indicator unit using a
display storage tube can be substituted for the standard
indicator. The bright display tube allows the pilot to read scope
information without the use of a hood under bright
light conditions. In this way, the pilot can read the radar
indicator as he would the flight instruments.
GENERAL
Radar System Complement - 5 major units (6
with two indicator operation)
Overall Weight-not installed - Approximately
125 Ibs.
Multiple Indicator Operation - Maximum of
two Indicators may be used
Bright Display Indicator - The system is
designed so that the Bright Display Indicator may be substituted for the
standard indicator without changes to the equipment or aircraft wiring
Primary Power
600 VA of 115 volts AC ± 5'10, 380 to 420 cycles
375 VA of 115 volts AC ± 10'10,380 to 420 cycles
30 watts of 27.5 volts DC
Operating Frequency-5400 mcs ± 30 mcs
Ranges-20-50-150 nautical miles
Altitude - Antenna--45,000 ft.; all other
units 16,000 ft.
Temp. Range - Antenna-40° C to +70° C;
all other units -40° C to +55° C
Gyro Information
System designed for antenna stabilization using gyro information as
supplied from Eclipse Pioneer PB I 0, PB20 or Sperry A 12 AutoPilot gyros.
CAA type certificated, 4R56-1.
RECEIVER· TRANSMITTER
Size-One ATR
Weight-43.75Ibs.
Mounting-Shock mounted plug-in unit with
"quick-disconnect" Waveguide connector
Power Output-75 KW peak
Pulse Width - 2.0 microseconds
Repetition Rate - 400 cycles (synchronized
with line frequency)
Magnetron Operation Time Delay - 5 minutes
ACCESSORY UNIT
Size - One ATR
Weight - 33 Ibs.
Mounting - Shock mounted plug-in unit
Range Marks - 5, 10, 25 mile spacing.
ISO-Contour Separation - Adjustable over
range of 5 db to 20 db
ANTENNA
Reflector Size - 22", 30", and
34"
Weight - 25 lbs.
Mounting - Unshockmounted plug-in unit
with "quick-disconnect" provisions for waveguide and power
connectors
Scan Rate - 15 rpm
Type Scan - 360° continuous
Type Stabilization - Line-of-Sight
Antenna Pattern - 7° horizontal beamwidth
with 22" reflector
Polarization - Fixed horizontal
Tilt - Up 10° down 15°
Stabilization Accuracy - ±2° (under
conditions of 0° manual tilt) during pitch and roll of aircraft, up to
±20° total excursion (for roll rates up to
20°/sec).
INDICATOR UNIT
Size - 61/4" sq. front with %"
radius corners x 13112"
Weight - 13 lbs.
Mounting - Shock mounted
PPI Tube - 5" diameter
Controls - The following controls are
provided on the front of the Indicator: CURSOR, INTENSITY, LIGHTS and
RANGEMARKS
BRIGHT DISPLAY INDICATOR UNIT
Size - 6 1/4" square front with
3/4" radius corners x 14112"
Weight - 15 lbs
Mounting - Instrument panel, shock mounted
PPI Tube - 5" Diameter
Controls - INTENSITY, RANGE MARKS, ERASE
RATE, and variable polaroid filter
CONTROL PANEL
Size - 33/8"x5%"x4112"
Weight - 2 lbs
Mounting - Unshockmounted plug-in unit
Controls - The following controls are
provided for selection of all system functions: OFF - STANDBY - RANGE -
switch, TILT control. GAIN control, CONTOUR control, and STABILIZATION
IN-OUT control
Edge Lighting - Edge
Lighting is provided for night time use. (A kit of pa,rts is available for
custom construction of control panels)
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(From: THE DISPLAY OF WEATHER ECHOES ON 5.5 cm AIRBORNE
RADAR UAL METEOROLOGY CIRCULAR No. 39 UNITED AIR LINES INC. DENVER,
COLORADO March 15, 1956 Henry T Harrison, Superintendent of Weather
Service Flight Operations Department.)
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THE DISPLAY OF WEATHER ECHOES ON THE
5.5 cm AIRBORNE RADAR
1. INTRODUCTION
This Circular presents additional meteorological results of three years
of flying tests and ground studies of the prototype and pre-production
model 5.5 cm airborne weather mapping radar built for United Air Lines by
Radio Corporation of America under specifications laid down by the Air
Transport Association and by Aeronautical Radio, Inc. While the original
UAL report in 1954* covered the general results of the 1953 flying tests,
this present report will discuss the nature and significance of weather
echoes in greater detail. The pictures were selected from the UAL file of
four radar catalogs which now contains more than 8,000 radar scope
photographs - all fully identified and correlated with the associated
weather situation.
Source of Data
While written primarily for meteorologists, the material in this report
should prove useful as a detailed reference source for flight personnel
and flight dispatchers as well, to supplement the radar course and
training literature received by them from the Denver Flight Training
Center. It would be well for the reader to bear in mind that all of the
pictures described herein were taken at flight altitudes which ranged from
500 feet above the ground up to a maximum of 15,500 feet msl, or were
actually taken while the radar was operating on the ground at Denver.
Since uptilt was used on the radar antenna in nearly all cases, it is
believed that the diagnosis of each echo should be valid for other
airborne radars operating at flight levels up to about 20,000 feet. Above
this level, and certainly above 25,000 feet, it is possible that the
significance of the storm echoes will have to be reappraised in a year or
two in the light of subsequent experience with the radar at higher levels.
A separate section will be included on this point near the end of the
report.
Comparison With Other Radars
The analysis of the C-band radar echoes will not necessarily be valid
for the same echoes dis
*''Evaluation of C-Band (5.5cm) Airborne Weather Radar." 1954.
UAL publication.
played on radars operating on the 3.2 cm band (X) , the 10 cm band (S)
or the 23 cm band (L); in fact, it is certain that they will not be
comparable in many instances because of the inherent differences of each
band with respect to attenuation, resolution, and sensitivity
characteristics. More and more we are beginning to realize that the
diagnosis of a particular radar weather echo ,is dependent to a very great
extent upon the type of the radar producing the picture. Even assuming
that each radar operator tunes his antenna-gain-brilliance controls for
optimum performance, there are still three factors which must be
considered in all cases before the real meaning of the radar observation
can be determined. These factors are:
1. Wave length of reporting radar.
2. Beam width.
3. Power output.
Since RAREPS distributed over the various teletype circuits may
originate from almost any type of radar from .8 cm up to 23 cm in wave
length, using antennas varying from about 18 inches up to more than 30
feet in diameter, or with power outputs varying more than tenfold, flight
operations personnel in the field are sometimes faced with a confusing
problem in trying to interpret the reports. The .8 cm radar, described
somewhat facetiously 'as being capable of "seeing your breath,"
is nearly useless under rain conditions. Certain powerful 3.2 cm radars
such as the Air Force CPS-9 are known to be capable of painting echoes on
fair weather cumulus clouds, but suffer attenuation and distortion of
picture when penetrating heavy rain. *
Powerful 10 cm sets, using antennas six feet or more in diameter,
produce a sharp picture with minimum of attenuation even under excessive
rainfall rates, but they are obviously unsuited for airborne application
because of the power and antenna requirements. Theory and actual tests
demonstrated that the six-centimeter band offered the most prac
*''The Use of Radar in Weather Forecasting With Particular Reference
to Radar Set AN/CPS-9." MIT Technical Report No. 20. By Hal Foster.
1952.
2 Weather Echoes on 5.5cm
Airborne Radar
tical compromise for obtaining maximum sensitivity with minimum
attenuation of signal in an airborne set. It was because of these
considerations that 5.5 cm was adopted as the optimum operating wave
length for airline airborne equipment by the Air Transport Association and
Aeronautical Radio, Inc. Pre-Production Model Display vs. the
Production Model Display
All pictures contained in this report were taken of the original
prototype 5.5 cm set built for United by RCA in 1953 and as modified
several times during the three years of testing operations by UAL
electronic technicians Frank Todd and David Clark. It is already apparent
to everyone who has worked with the new production model that the picture
on the field radar is perceptibly sharper, the contour display is
superior, and the range of reception of all echoes is greater. The first
new set installed in the MAINLINER "O'Connor" picked up several
thunderstorm echoes on the outer range mark of the 150-mile range during
one of the Denver Flight Training Center Project flights to Redwood Falls,
Minnesota, on July 7, 1955. The improved picture is the result of
engineering refinements built into the new set by RCA engineers working
closely with United's own electronic technicians.
Another difference to keep in mind is that the line radar scope will
have the writing beam centered 25 % below the geometrical center of the
scope. This point was adopted after several experiments as the most
practical compromise in giving the pilot maximum blowup of the picture
ahead of him with minimum loss of picture to the right and left of the
plane.
How To Read The Scope Photographs
1. In the aerial pictures, 12 o'clock is always straight ahead of the
plane. Heading is indicated by the compass figure (magnetic) in the slot
at the edge of the scope at 11 o'clock.
2. In the ground pictures taken in the airplane, the direction the
plane is facing is also indicated by the compass figure in the slot at 11
o'clock.
3. In the ground pictures taken with the radar in the final roof
position at the Operating Base, the scope is map reading with true north
at 12 o'clock and east at 3 o'clock.
4. The effective sweep of the scanner is limited to about
2400 in all pictures taken while the set was
installed in the airplane.
5. A full 3600 scope picture appears in all photo graphs
taken with the radar on the roof installation.
6. Date and flight number appear in the lower left. 7. Range marks may
be identified by the number which appears on the
scope. 5 marks visible signify 2-mile intervals, 6 marks are 5-mile
intervals and 4 marks are 25-mile intervals.
8. Since the scope was photographed in a mirror, the clock prints as an
inverted mirror image. 9. All radar photographs were taken with a
PERISCOPE, RECORDING CAMERA (TYPE 0-5) TYPE A-1, SERIAL 275 SPECIFICATION
NO. R-31409, ST. GEORGE RECORDING EQUIPMENT CORPORATION, NEW YORK CITY.
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(There are many many pages of photographs of
the scope face showing formations these are not present here
on this web page.) |
94 Weather Echoes on
5.5cm Airborne Radar
APPENDIX
A BRIEF HISTORY OF THE DEVELOPMENT OF AIRBORNE WEATHER RADAR
Note
(Much of the material contained in this abbreviated history was
presented as part of the third annual report of the AT A Meteorological
Subcommttee to the Operations Conference at WiIIiamsburg, Virginia, on
June 15, 1955. The special committee charged with preparing this report
consisted of H. T. Harrison of UAL (Chairman), R. H. Curtis of CAL and J.
A. Browne of TWA. Presentation was made by Harrison.)
WORLD WAR II
To pick up the thread of the airborne weather radar story, it is well
to recall that the display of weather echoes grew up quite accidentally as
an unintentional by-product of military radars which were designed for
bombing and navigation purposes near the start of World War II. When it
was discovered that radar could see water drops about as well as it picked
up ground targets, meteorologists were quick to recognize the enormous
potentials of this new instrument as a weather observing and forecasting
tool. Almost overnight, we were in the fortunate position of being able to
X-ray thunderstorms, hurricanes and general storm areas to complete the
third dimension picture which had been missing up to that time.
EARLY TWA RESEARCH
Near the end of World War II, considerable interest was focused on the
possibility of installing cockpit radar in airline planes for storm
avoidance purposes. Trans World Airlines in late 1945 and 1946 had a close
look at a 3.2 cm airborne set which was built especially for them by Bell
Laboratories and Western Electric from components taken from war surplus
equipment used by the military. Subjected first to a series of tests on
the ground in the TWA Weather Office at Kansas City for three months, the
radar was then installed in a C-47 plane for a series of flight checks.
While the immediate results of this project were somewhat disappointing,
the TWA group under Ralph Ayres was enthusiastic over the possibilities
and recommended that future airborne search radars should be developed
specifically for storm avoidance. J. A. Browne, Manager of Meteorology for
TWA, took an active part in all of the ground tests and some of the flight
research.
AAl PROJECT
American Airlines, operating under a Navy contract, was another
pioneering airline to conduct a major project looking into the application
of airborne radar. The American group did some excellent work in
correlating 3.2 cm radar pictures with I FR penetrations of actual
thunderstorm conditions, including the development of a highly practical
application of the principle of providing a second rainfall rate contour
for the purpose of painting in the heavy rain cores of storms. This
attachment was first known as ISOECHO CONTOUR CIRCUITRY, but has gradually
been shortened to the simple term CONTOUR. Among those participating in
this project were: Don Beard, A. F. Mereweather Superintendent of Weather
Services for American, Frank White- (now with ATA), and Sam Saint who is
now with ANDB after a tour of duty with AT A. This project was also
credited with developing the principle of correlating heavy thunderstorm
turbulence with sharp edged radar echoes, possibly the greatest
contribution of all in the developmental history of airborne weather
avoidance radar.
NAVY PROJECT
The Navy conducted another airborne radar project in 1949 and 1950 with
one of the main purposes being to determine the possibility of identifying
hail shafts on the 3.2 cm radar. Commander Earl Perce and Lt. Montgomery
were the pilots and Frank White again took part in this project as radar
officer, this time on active duty as a Navy Reservist. Joe George,
Superintendent of Meteorology for Eastern, served on this project as
Weather Observer while on active duty as a Brigadier General in the Air
Force Reserve. Winding up in Denver during June 1950, the ruggedness of
these tests is shown by the fact that hai I damage to the plane was severe
enough to force cancellation of further flight testing.
WEAKNESSES OF WARTIME EQUIPMENT
In spite of the early post-war enthusiasm, it soon became evident that
there was a major obstacle standing in the way of immediate adoption of
airborne radar by the airlines. This was the unsatisfactory nature of the
available equipment which had been built for military use and primarily
for purposes other than storm avoidance. The equipment was heavy, it was
subject to frequent breakdowns and - because it operated on a wave length
of 3.2 cm - it produced seriously distorted pictures whenever the beam
penetrated heavy rain or whenever the plane was flying in heavy rain. In
short, the 3.2 cm radar was a useful piece of equipment for detouring
storm areas, but appeared to be undependable for penetrating corridors in
lines of thunderstorms on the airway.
Appendix 95
ATA-ARINC SPECIFICATIONS
It was not until May 1, 1952, that ATA came face to face with the
problem by taking positive steps to break the bottleneck. On that historic
date, a group of interested ATA members drew up a set of ten operational
requirements which was then submitted to the Airlines Electronic
Engineering Committee under the chairmanship of Frank Todd of United with
orders to convert the requirements into technical characteristics. The
most critical of these requirements was the one pertaining to attenuation
of the radar by heavy rain:
"3. The equipment must be capable of penetrating and displaying at
short range rainfall rates of 60 mm/hr to a depth of 15 miles."
THE McGill STUDY
This ATA-ARINC requirement practically ruled out consideration of 3.2
cm as the wave length for the standard airline radar in the United States
by virtue of its well known attenuation characteristics at lesser rainfall
rates. To make doubly certain on this point, however, AT A and ARINC
contracted with McGill University to carry out a theoretical study to find
the most practical wave length for airline radar, keeping in mind the
limitations imposed on the equipment by the size of the antenna dish and
the available power supply in the typical modern transport plane. The
McGill study, produced by J. S. Marshall and Walter Hitschfeld, contained
the following conclusion:
"That an operating wave length of 5.5 cm will provide optimum
performance for weather mapping radar from the standpoint of providing
maximum sensitivity with minimum attenuation of signal in heavy
rain."
FIRST PROTOTYPE TO AIRLINE SPECIFICATIONS - THE UAL PROJECT
Shortly after the AEEC specifications were announced, one manufacturer
- Radio Corporation of America - contracted with United to build a
prototype radar to meet all of the airline specifications. Delivered in
Denver June 1, 1953, this completely new C-Band radar was subjected to a
series of 40 flight tests by United in thunderstorm conditions over the
Western Plains during the summer of 1953 with the results being reported
in the UAL publication, "Evaluation of C-Band (5.5cm) Airborne
Weather Radar." When these tests demonstrated that the prototype
radar met all of the AEEC specifications satisfactorily, the United
evaluation team recommended that the company purchase this type of radar
for fleet installation.
FIRST PRODUCTION 5.5 CM MODELS
Two manufacturers - RCA and Bendix - submitted pre-production 5.5 cm
airborne radars to United ,in January and February of 1955 for bench
testing by the Communications and Engineering Departments in Denver and
San Francisco respectively. These tests culminated in the placing of an
order by United with RCA on 4/5/55 to equip the entire UAL fleet with
C-Band radar. All UAL Convairs will be operational by the spring of 1956,
all DC-6's and DC-7's by the fall of 1957. As of the present writing,
practically every airline in the country has placed orders for airborne
radar with a majority calling for C-Band equipment. A third manufacturer,
Collins Radio, has recently entered the airborne radar production field
with a 5.5 cm radar built to ATA-ARINC specifications.
ADDITIONAL UAL GROUND TESTS
Pending delivery of the final production models, ground observations
were continued by United on the original prototype set at Denver starting
in the spring of 1954 with the radar still installed in the DC-3 airplane.
In September 1954 the set was transferred to a permanent location in the
Weather Office at the Operating Base with the transmitter/receiver and
power units being installed in an aluminum house on the roof and the
antenna shielded by a masonite radome immediately above. Observations have
been almost daily with the set ever since, including pictures of the scope
whenever interesting weather developments took place. The original
prototype was replaced with a production model RCA AVQ-10 5.5 cm radar in
October 1955.
The United catalog now includes pictures of wet snow, dry snow, steady
rain, rain and snow showers, hail, thunderstorms, terrain and anomalous
terrain echoes. It also includes a number of radar pictures taken of
thunderstorms where small tornadoes were reported by ground observers, but
these pictures have shown little in the way of a useful correlation to
identify the tornado on the scope. (More on this subject in Section 7 of
this report.) There are now more than 400 pictures of hail shafts which
started with the 23 flights in 1953 where hail was known to have occurred,
followed by ground observations of hail shafts on 8 days in 1954 and 11
days in 1955. All pictures are fully identified and are
available quickly for study and reference by any interested persons.
96 Weather Echoes on 5.5cm Airborne
Radar
APPENDIX II
COMPARISON OF SPECIFICATIONS OF ORIGINAL RCA
PROTOTYPE
AND THE 1955 PRODUCTION 5.5 CM RADAR |
Specification |
Prototype 1953 |
AVQ- 10 1955 |
Operating wave length |
5.5 cm |
5.5 cm |
Antenna diameter |
Antenna diameter22" parabola |
22" or 30" ellipse |
Beam width |
7.5 |
5.4 with 30" dish |
Rate of scan |
15 or 40 rpm |
15 rpm |
Antenna tilt |
-150
to +90 |
-150
to +100 |
Antenna stabilization |
Roll |
Roll and pitch |
Scan |
3600
continuous |
3600
continuous |
Power output |
53 kw |
75 kw |
Indicator scope |
Center PPI |
25% off-center PPI |
Scope brightness |
Viewing hood |
Viewing hood |
Scope ranges |
Scope ranges10 - 30 - 100 |
20 - 50 - 150 |
Range marks |
2 - 5 - 25 |
2 - 5 - 25 |
PPI tube diameter |
5"5" |
5"5" |
Over-all weight |
200 pounds |
116 pounds |
Iso-contour attachment |
Yes |
Yes |
Iso-contour ratio |
5 to 20 db |
5 to 15 db |
Circular polarization |
Yes |
No |
Sensitivity time control |
Yes |
Yes |
Magnetron warm-up period |
8 minutes |
4 minutes |
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APPENDIX III
BIBLIOGRAPHY OF UAL RADAR
PUBLICATIONS AND TRAINING AIDS Films
"The Adventures of Sir Echo." 1953. A 50-minute
documentary moving picture of the radar flight tests of 1953 in 16 mm
color. Produced by M. E. Balzer. Radar echoes and cloud exteriors are
shown side by side with running sound commentary by Balzer.
"United's New look." 1955. A 40-minute pilot training
moving picture in 16 mm color produced by Thomas J. Barbre Motion Picture
Productions of Denver under the technical direction of M. E. Balzer and F.
J. Todd. Motion picture sequences are shown of the actual scope in
operation on board the Mainliner O/CONNOR while approaching and
penetrating thunderstorm conditions. Running sound commentary by Balzer.
Copyright UAL.
"UAL Training Film No. 1." 1955. A 10-minute
supplementary training moving picture designed for use as a final
examination of pilots at end of training course. 16 mm block and white.
Silent. Copyright UAL.
Other Classroom Aids
Classroom Slides. 72 Vu-Graph transparencies of radar scope
pictures. Developed by M. E. Balzer. 10-inch size. Complete with lecture
outline and notes. Copyright UAL.
Radar Home Study lesson For Pilots. 1955. Section of revised UAL
Home Study Course in Meteorology. Prepared by M. E. Balzer and H. R.
Hoffman. Copyright UAL.
UAL Radar Catalog. 1953- 1956. Four volumes containing
approximately 8/000 glossy prints of scope pictures correlated with
associated weather conditions. Original film negatives and 35 mm slides
also available.
Technical Papers
"The Operational Applications of Airborne Radar."
1954. By E. A. Post.
"Application of Airborne Radar To Airline Operations."
1954. By E. A. Post.
"Airborne Weather Radar Evaluation." 1954. UAL
COCKPIT. 9-54. By E. A. Post.
"The History of Modern Airline Radar - Its Development,
Performance/ Application, and Installation." 1954. By F. J. Todd.
"The Display of Hail Echoes on 5.5 em Weather Mapping
Radar." 1956. By H. T. Harrison. 20 illustrations.
Book-length Reports
"Evaluation of C-Band (5.5 cm) Airborne Weather Radar."
1954. By H. T. Harrison and E. A. Post. Official UAL report on results of
40 flight tests in 1953 using the RCA prototype radar. 108 pages.
Illustrated.
"The Display of Weather Echoes On The 5.5 cm Airborne Radar."
1956. UAL Meteorology Circular No. 39 by H. T. Harrison. 250
illustrations.
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RCA AVQ-10 Weather Radar Movie |
RCA AVQ-10 Weather Radar Movie
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Be sure that you have allowed active content
when this web page loaded to watch the movie! |
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RADIO CORPORATION OF AMERICA AVQ-10
Ad from 1958 RCA Electronic Age Magazine
RCA ELECTRONICS KEEPS A RADAR
"WEATHER EYE" ON YOUR COMFORT ON THE GREAT
AIRLINES
Airlines equipped with RCA all weather radar include: United Air Lines
(DC-7 above), Trans-World Airlines, American Airlines, Continental
Airlines, Pan American, Braniff, CAA, Air France, Cia Mexicana, Swissair,
Sabena, BOAC. Iberia, RAAF, Air India, Qantas, Cubana, Karhumaki, Real-Aerovias,
TCA, Japan Air Lines, Panair Do Brasil, Swedish Nabel Beard, Pakistan
Airlines, SAS, Thai Airways Ltd., Ethiopian Airlines, Olympic Airlines.
Flying into a starless night, the pilot's vision may reach a mere 50
yards. Yet he sees a storm brewing 150 miles ahead. Within minutes he
plots a slight change in course and has a smooth, safe corridor through
the weather. His passengers complete their trip in comfort and on
schedule. Credit RCA Electronics for the "Weather Eye" radar
that makes all this possible. And United Air Lines' all-radar Fleet for being
first (among 24 leading airlines) to use this important development.
RCA has also produced radar to guide ships at sea, and track man-made
satellites through space. RCA pioneered and developed color TV, produced
the world's largest electronic computer, peanut-sized transistors and
much, much more.
Progress like this helps explain why RCA means electronics and why
electronics means a happier, healthier, more secure future for you. |
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Radar
Sees The Weather
From the 1981 KOY Almanac By Ed Phillips, and when Ed changed
employment, later to be published by KTAR. This was page 40. We have this
AVQ-10 Radar
The word radar means Radio Detection And Ranging. Simply put, a radar
is a device used to detect distant objects that reflect radio energy.
Since only objects that reflect energy show up on the radar screen, they
are called "echoes."
In the case of a weather radar, the energy is reflected because of
precipitation, not clouds, aircraft or dust. This feature enables the user
to 'see' within the clouds and find out if they are producing rain or
snow. The rain and snow echoes are displayed on a screen much like a T.V.
picture. From the location on the screen, the operator can determine the
direction and distance the rain is away from the radar unit.
The KOY Weather Station is equipped with weather radar. An RCA AVQ-10
Aircraft Radar has been modified for stationary operation. With our radar,
the strongest storms can be seen 150 nautical miles away. The distance you
can see rain is of course limited by mountains and buildings because the
radar signal travels in a straight line. Our radar set also has a fifty
mile range. We use it most often because it gives good coverage to all of
the Salt River Valley. A 20 mile range is also available to use when
storms are in close range. We operate our radar any time rain is
threatening the valley. KOY is the only broadcasting station in the valley
that has weather radar. Radar updates are given every half hour during
morning and afternoon drive times when there is rain around. If severe
weather threatens, you can count on us to have the storms pinpointed and
keep you abreast of the latest weather developments.
40
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