© Brooke Clarke, N6GCE 2001 - 2020
AGM-77 Hound Dog Azimuth Alignment prior to launch.
fits in 16x16x16" box
Display Panel, Star Data
Three Start supported, so 3 display panels
showing the location of each star.
Azmith & Ground Range
s/n AF57 132
33 600 31502
screw on shell
30 male pins
1 1/8" ID
Display Panel, Star Data J1401 120
HS Feb 6 1959
SHA: 2h 31m 49.09s
DEC: +89d `5' 50.9"
So the display is not Polaris now
Automatic Astro Compass Type MD-1
Stock No. 6225-A21570 00 004
Serial No. AF57-1308
Part No. A21570 00 004
Contract No. AF33(600)-33105
Kollsman Instrument Corporation
30 male pins
1 5/16-6 Acme
30 male pins
30 male pins
3 each photo multiplier?
33 in Hg
Bubble level vial
Automatic Astro Comapss Type MD-1
Stock No. 6605-658-2565
Serial No. AF61-2136
Mfrs Part No. A21570 ?004
Contract No. AF33(600)-42020
Kollsman Instrument Corporation
Side Top Raster
The Manual Astro Compass was replaced by the periscopic sextant which was replaced by the automatic astro-compass. This may have been the first in a series of star tracking instruments used in aircraft, missiles and space craft.
There are two very similar astro trackers, the C2150 00 003 and the D21550 00 001, what the difference is is unknown.
I have been told this is a part number A2157000004 with NSN 6605-00-658-2565.
The part number D2155000001 version has a NSN of 6605-00-776-3234.
||Lancaster, Halifax, B-17,
|Mk II Astrocompass
|MD-1 Automatic Astrocompass
||B-52C, B-52D, B-52E,
|Kollsman Inst KS-140 Auto
||NAA AGM-28A Hound Dog Missile|
AF33(657)-12897, AF34(601)-25601 (T.O. 5N1-2-17-1, KS 50-08)
|B-52H (later), RC-135
||FB-111A through the
FB-111F, removed in the FG-111G
Stellar Internal GPS Nav
||RC-135 V/W Rivet Joint
Project 621 (1962) & NRL TIMATION project (1963) led
to Satellite Nav Systems replacing most star trackers
See: Milestones Stellar Navigation to satellite Navigation by Dr. Carlo Kopp
Also see: Sputnik, Transit & GPS
R. S. maintained the MD-1 from 1967 through 1970, which includes the Viet Nam era. 18 Dec. 1972 bombing of N. Viet Nam was allowed. The Arc Light missions were flown from Thailand, Okinawa and Guam using B-52s with MD-1 capability. Nixon was a football fan and he named a later mission "Linebacker".
The MD-1 was used on the B-52 C & D as well as in the E and F variants. Many of the boxes that made up the MD-1 system were located in the right forward wheel well. Subjecting them to problems from slush from wet runways. One of the problems was the tuning fork that drives the clock would die. Being an analog system you could not just replace the tuning fork box, but also needed to adjust a number of pots.
Another problem in the states was when a chew chief would scrape ice off the B-52 they would sometimes also scrape off the dome of the MD-1 and ask to have the dome replaced. Well you can't do that, the whole MD-1 needs to be replaced and properly leveled.
The Hound Dog missile that was carried on the B-52 also used a smaller version of the astro tracker. Sometimes when the about 2 foot diameter MD-1 astro tracker was ordered, the one foot diameter astro tracker for the Hound Dog would be delivered.
There was a star simulator that had 3 "stars" in known locations that could be used for testing the MD-1 system. When testing at night mag 1 stars were used since they were easier to lock onto.
Lighting bugs were not a problem. Most of the time when a problem ticket on the MD-1 showed up it was do to lack of training, rather than equipment failure.
There are B-52s on static display, that should have MD-1 systems at: Travis, Castle, March and Edwards fields in CA.
Hisory, AF Plant Representative, Boeing Airplane Co. July - Dec. 1958 by Col. Robert E. Lee
Unclassified CMS 0476305
This report contains sections for:
Quality Control -
The MD-1 Astro Compass continued to be a source of trouble. It was discovered that several of the small plug-in amplifiers had bent pins and socket damage due to misalignment of the sockets in the unit. However, this problem appears to have been cleared up by the vendor at this time.Production - B-52G engineering was moved from Seattle to Wichita completed by 31 Dec. 1958.
Another problem of the MD-1 System was the inaccuracy of the clock used with this equipment and the fact that there was no flight test tolerance for the clock. this condiditon was alleviated with the issuance of a flight tolerance and the installation of a new Tuning Fork and Time Standard Amplifier.
Flight Operations and Acceptance - 143 B-52 flight tests for 459:10 hours.
Finance and Accounting
Contracts - B-47 Project: Milk Bottle, B-52 Projects: Wheat State, Harvest Moon
Photoss - refuling During Maiden Flight of B-52G Stratofortress, zB-47 Stratojet in Water Injection Take-off.
Control PanelsThe capabilities of the system were classified. That's why the displays and some of the controls in the following images have been sanitized.
Display Present Position Display Star Data for 3 stars
Display Aries GHA & UTC
Lower instrument is a clock
Choose how to set
assumed Lat Lon
Display True Heading
Display True Azmith
Must allow setting 3 star positions
& present position
In addition to the above control panels there are 10 other ATR type boxes with the analog computer and other electronics boxes that make up this system.
In this version an automated Star tracker looks out a clear astrodome on the top of a B-52E/F and tracks either a star or the Sun. There were a number of star trackers built for many programs both for aircraft, missile and space craft navigation.
AF manual 51-40 Volume 3 Air Navigation (15 Apr 60) has a couple of pages on the MD-1: Cover, Part 1, Part 2, mentions "minutes of arc" accuracy. Done using an analog computer. Photographs of the instruments are not sanitized, so you can see more than on the photos above. This is just 2 years after the classified paper above and the capabilities are no longer classified.
WANTED - Manual with schematic and/or theory of operation diagram for the star tracker
By inspection of the parts manual T.O. 5N15-2-2-4 some things can be learned. All of the parts listed below need some type of electrical connection. There is a minimal amount of electronic content inside the star tracker.
T.O. 5N15-2-2-507 contains a modification that improved the operation of the MD-1. It is applied to the 3 kHz raster assembly p/n 85 21552 0370. This implies that there is an X-Y scanner in the system and would explain some of the active components above and the use of audio transformers.
- a single photomultiplier (fig 5-27) is used that looks like an octal based vacuum tube, maybe a 931 photomultiplier (Burle).
- the telescope assembly sits on a roll-pitch correction assembly that has maybe +/- 8 degrees range (T.O. 5N15-2-2-505)
- the telescope assembly includes parts to aim in azimuth(rotation) and elevation (tipping the prism) but what are the rest of the items are for?
Astro Trracker Major Assemblies Fig 2
- 2-9 Vertical gyro - is external to the astro tracker (available from C&H Sales )
- 2-47 Telescope Fig 3 - contains the optical tower, prism and underneath the tracker and photomultiplier
- Telescope sub-assembly Fig 4 - just the optical tube
- Tracker sub-assembly, photoelectric cell Fig 5 - metal casting that holds the photomultiplier, 2 ea transformers, cover that allows light into the center of the tube along the long axis.
- Gear Box Tracker sub-assembly Fig 6 - larger in diameter than the telescope with many electrical feed-through terminals around the outside. has the "raster".
- 6-17 synchro control transformer B106
- 6-18 induction generator Fig 7 MG102
- 6-28 synchro control transformer B104
- 6-35 synchro resolver B105
- 6-48 synchro control transformer B103
- 6-49 induction generator Fig 7 MG101
- 6-60 potentiometer, secant
- 6-67 synchro control transformer B102
- 6-71 synchronous motor Fig 9 B101
- 6-78 permanent magnet generator Fig 10 G101
- 6-135 Differential Assembly Fig 11 (no electrical parts)
- 6-173 solenoid L101
- 2-62 Blower, minicube B111, B112, B113, B114
- 2-94 Roll Drive gear Box
- 12-12 induction generator (induction motor?) Fig 14 B109
- 12-13 induction generator Fig 15 G103
- 12-17 magnetic brake assembly Fig 16 L102
- 12-3 (2 each) switching circuits that contain an audio transformer Fig 13
- 2-98 Roll Synchro Gear Box Fig 17
- 17-20 synchro control transformer B110
- 2-102 Pitch Synchro Gear Box Fig 18
- 18-21 synchro control transformer B108
- 2-105 Pitch Drive Gear Box Fig 19
- 19-1 magnetic brake assembly L105
- 19-5 induction motor B107
- 19-9 induction generator G102
- 2-133 Pitch Gimball assembly Fig 20
- 2-134 Roll Gimball assembly Fig 21
- 2-136 Platform assembly Fig 22
many with class 250/203.6
The original idea was to just track a single star when it was dark out. Then a problem surfaced at dawn and dusk there is an East West gradient in the sky background that causes an error in the early type star trackers. A number of solutions were found. The next step was to have a star tracker that would track a star in daylight. This requires optimizing the signal to noise ratio in the complete system.
Three of the patents below are assigned to Kollsman, but which of any apply to the MD-1 remains to be seen.
6236939 May 22, 2001 Method and apparatus for controlling spacecraft attitude with rotational star trackers
6047226 April 4, 2000 Enhanced stellar attitude determination system
5525793 June 11, 1996 Optical head having an imaging sensor for imaging an object in a field of view and a tracking sensor for tracking a star off axis to the field of view of the imaging sensor - Santa Barbara Instrument Group
4159419 June 26, 1979 Three axis stellar sensor
3936632 February 3, 1976 Position determining system - star tracking for satellites 250/237R; 250/203.5; 250/203.6
3578975 May 18, 1971 Apparatus for Monitoring the Guidance and Focus of Telescope
3310877 Vehicle optical alignment device - on the importance of keeping the optical center of the periscope centered in the glass hemisphere to avoid distortion
3295010 Image Dissector with Field Mesh near Photocathode, ITT
3287562 Photosensitive scanning means for rotating an image with respect to a light modulator,
Jr James J Connors, J ohn W Barnes,KOLLSMAN INSTR CORP, 1964-02-28 -
3246160 Photosensitive horizon scanner for space vehicle, Jacob S Zuckerbraun, KOLLSMAN INSTR CORP, 1966-04-12 - two circles with offset centers form the pattern.
3244896 Star tracker scanning system using a circular scanning pattern and a square aperture, Walker Burt, KOLLSMAN INSTR CORP, 1962-12-14 - with a square sensor the star image appears in all 4 corners, when it moves off center one of those images goes away indicating the direction of movement.
3165632 Jan 12, 1965 Star-Tracking System using a Frequency Modulated Carrier Wave, defective USPTO pages
3131249 April 28, 1964 Stellar Compass, Karolus Kunze,
3127516 March 31, 1964 Star Tracker having adjustable scan dependent upon radiation intensity, bad USPTO pages missile?
3122644 Feb 25, 1964 Binocular Star Sensing System, William B Greenlee, Victor A Miller, North American Aviation, star position in the presence of gradient background illumination
3117231 Jan 7, 1964 Optical Tracking System, U.S. Navy, sidewinder IR tracker?
3100264 Aug 6, 1963 Star Energy Identification System for Space Navigation, Polarad Corp, amplitude frequency absorption spectrum used to identify objects in space for satellite navigation.
3088033 April 30, 1963 Automatic Multiple Grid Scanning Tracker, Northrop day & night star tracker
3080485 March 5, 1963 Stellar Orientation Monitoring System, HRB-Singer, a motor scans a photo multiplier and the star pattern is recorded and compared in future scans, for missile navigation
3080484 Mar 5, 1963 Electrooptical Light-Detecting Apparatus, Hughes, day or night star tracking, uses narrow band filtering requires constant frequency, not frequency modulation like in nutating systems, this is a switched system aimed at missile navigation
3072794 Jan 8, 1962, Northrop, Rotating Wheel Scanner for star tracking
3053984 Sept 11, 1962 Star Tracking System, defective USPTO pages
3042296 Celestial Data Computer, V.E. Carbonara & E.D. MacDonald (Kolsman Inst Corp), Jul 3, 1962, 235/61NV - part of MD-1?
3037289 June 5, 1962 Directional Reference Correction System, Sperry Rand, math for making star tracking corrections
3024699 Light modulation system,
Anwar K Chitayet, KOLLSMAN INSTR CORP, 1962-03-13 KOLLSMAN INSTR CORPKOLLSMAN INSTR CORKOLLSMAN INSTR CORPKOLLSMAN INSTR CORPKOLLSMAN INSTR CORP 3015249 Jan 2, 1962 Tracking Telescope, Northrop, automatic star tracker
3014133 Dec 19, 1961 Star Tracker, United Aircraft, submarine periscope
3022703 Optical Navigation Device, M.R. Pierce, Feb 27 1962, 356/143; 356/140; 356/147 -
3006236 Apparatus for astronomical navigation, Michaud Robert A H (Sud Aviation), Oct 31, 1961, 356/139.2, 356/139.5, 356/149, 356/147, 356/139.6 -
3002097 Sept 26, 1961 Dispersion Scanner, Northrop, star tracker with acceleration correction
3002096 Sept 26, 1961 Light Tracking Device, Kollsman, removes background illumination even when a gradient
2998529 Automatic Astrocompass (Kollsamn) (Sun in daytime, Star at night) 250/206.3 ; 250/203.1; 250/203.4; 250/207; 356/139.02 - part of MD-1?
2421012 Homing System (Navy) cylindrical lens and chopper 250/206.3 ; 102/213; 244/3.16; 250/203.1; 250/214.1; 250/215; 250/233; 318/480
2713134 Radient Energy Controller Followup System (Kollsman) reticle and PMT 318/575 ; 250/203.3; 250/203.7; 318/16; 318/489; 318/625; 318/640; 74/5.34
2981843 April 25, 1961 Star-Tracking System, Hughes Aircraft, works with a bright background
2961191 Automatic One-Star Navigational Directors, R.E. Japerson, Mar 1, 1957, 244/3.18, 244/175, 701/513 -
2957742 Automatic Course Follower and Recorder, V.E. Carbonara (Kollsman Inst Corp), Oct 25 1960, 346/8; 33/268; 318/582; 342/452; 346/112 -
2949030 Gyroscopically stabilized optical system platform, Jr Robert Bruce Horsfall, John M Slater, John A Widenmann, North American Aviation, App: 1949-04-09, Pub: 1960-08-16, - a gyro stabilized telescope for star sights to update an inertial nav system.
2948813 Aug 9, 1960 Tracking System, Aerojet-General, missile
2947872 Aug 2, 1960, Star Tracking System, Kollsman, (filed 23 Jan, 1956)
2943204 June 28, 1960 Star Sensing System, William B Greenlee, Victor A Miller, North American Aviation, daytime and multiple stars, rotating reticule
2942118 June 21, 1960 Radiant Energy Angular Tracking Device, Westinghouse, off center reticule is rotated
2941082 PhotoElectric Automatic Sextant (Kollsman) 356/139.01 ; 244/3.18; 33/268; 356/148 - probably newer than MD-1?
2444933 Automatic Navigational Director (Navy star tracker) 318/581 ; 244/3.18; 250/203.1; 250/348; 318/480; 318/640; 33/1SC; 701/222; 73/178R
2462925 Radiant Energy Directional Apparatus (R. Varian sextant that works in daylight) 318/640 ; 250/236; 318/480; 318/625; 33/268; 73/178R
2492148 Automatic Navigating Instrument for Craft Guidance (Sun or star) 318/582 ; 244/3.18; 313/531; 318/480; 318/577; 318/656; 33/1SC; 33/268; 33/320
2513367 Radiant Energy Tracking Device (Sperry) 250/203.6 ; 244/177; 244/3.18; 250/204; 250/233; 250/236; 318/582; 318/640; 33/1CC
2532402 Navigation Instrument for Craft and Pilot Guidance 318/581 ; 114/144E; 114/144R; 235/61NV; 318/577; 318/632; 318/675; 33/264; 33/268; 89/1.51
2533686 Gyroscopic Sextant (gyro replaces visible horizon) 33/275G ; 33/282; 33/318
2762123 Navigation System (Sperry) (celestial navigation) 33/1SA ; 235/61NV; 244/3.18; 250/203.6; 318/582; 33/268; 356/248; 701/221; 701/222; 74/5R; 74/5.34
3263944 Aug., 1966 Space Craft Navigation System
2941081 Stellar orientation detector, William B Greenlee, Victor A Miller, North American Aviation, App: 1950-09-27, Pub: 1960-06-14, - "...a star sensing system in which the effect of sky gradient signals is substantially eliminated."
2931910 April 5, 1960 Automatic Star Tracker, Northrop, rotating wedge with a 10 deg clear field (application 14 March 1949)
2930545 March 29, 1960 Automatic Celestial Navigation Control System, General Scientific Projects, objective prism, track 2 stars
2922224 Jan 26, 1960 Navigation System Employing Star Heading Reference, General Precision Labs, "star tracker" a rotating wedge causes a sin wave output of the spot of light is off center and a DC output when centered.
2921757 June 26, 1948 Long Range Automatic Navigator Device General Scientific Projects "Stellar Compass" 4 photo cells
2906916 Sep 29, 1959 Position Sensing Detector Du Mount Labs photo multiplier for missile homing
2905828 Light tracking device,
James B O'maley, John W Barnes, Paul D Hansell,KOLLSMAN INSTR CORP, 1952-11-20 - Spinning diak with pattern and PMT
2894396 7/1959 a gyroscopic unit
2829833 Azimuth Counter, Victor E Carbonara, KOLLSMAN INSTR CORP, 1958-04-08 -
2782675 Artificial horizon, Howard J Eckweiler, KOLLSMAN INSTR CORP, 1957-02-26 -
2762123 May 26, 1948 Navigation System - Spery Rand Corp - 3D gyro system with star tracker using photo multiplier tubes
2734269 Aug 11, 1952 Angular Position Data Apparatus - Ionoscope arc seconds accuracy
2713134 July 12, 1955, Radiant Energy Controlled Follow-up System, Kollsman, photo multiplier and 400 Hz rotating mask, automatic star follower
This appears to be the patent used for the MD1.
It calls the indented patents :2941081
2707898 Vertically oriented optical system (Zenith Star Source), Jr Robert B Horsfall, North American Aviation, 1955-05-10, -
2529619 Aerial navigation system, George A Maney, App: 1944-09-04, Pub: 1950-11-14, - double integration of acceleration to know position, i.e. inertial navigation
2462081 Feb 22, 1949, Servomotor System assigned to Sperry Corp (auto pilot for flying wing)
2462925 (Google) March 1, 1949 Radiant Energy Directional Device, Russell H. Varian, Palo Alto assigned to Sperry Corp
Can track stars during both night AND day! Automatic star tracking. The construction is based on a sextant.
This appears to be the first star tracker.
2369622 Orientation System, Feb 13, 1945, Toulon, automatic pointing to a source of energy (IR) like the Sun, mounted on a ship
2246884 Potentiometer, June 24, 1941, balanced control system for temperature indication
2155402 Sun Compass, April 25, 1939, Joseph C. Clark, true meridian indicator using motors and light sensitive sensors- uses vacuum tube photocells.
1963692 Light Sensitive Cell (Clark Cell), June 19, 1934, Joseph C. Clark, Selenium photo cell process for making - predates the Weston Photonic Cell patent 2000642.2102587 Solar Navigator, Dec 21 1937, Leon T. Eliel, use the Sun to fly an airplane in a straight line for map making.
1999646 Light or Ray Controlled Follow-up System, April 30, 1935, B. A. Wittkuhns assigned to Spery Corp. uses photo cells and motors
1976648 Remote control System, Oct. 9, 1934, B. A. Wittkuhns, to Spery Gyroscope, dual cathode photocell
2513367 May 25, 1948 Radiant Energy Tracking Apparatus, Sperry Corp, star tracking telescope2369622 Orientation System, Feb 13, 1945, Toulon, automatic pointing to a source of energy (IR) on a ship2505819 Panoramic Sextant having Stabilized Reticle, W. Wrigley (Sperry Corp), May 2 1950, 356/149; 359/401; 359/428; 359/429; 359/557; 359/725; 359/737 -
2397933 Line Tracker Control, Aprio 9, 1946, milling machine controlled by drawing
2313734 Temperature Compensated Bubble for Panoramic Sextants, C.J. Crane & S.M. Burka, Mar 16 1943, 33/315; 33/348; 33/379; 219/201 -
2262920 Illuminating Means for Instruments, V.E. Carbonara (Square D Co), Nov 18 1941, 362/30; 73/431; 362/267; 362/268; 362/339; 439/675 -
2280798 Panoramic Sextant, C.J. Crane & S.M Burka, Apr 28 1942, 356/147; 116/299; 356/148 - aircraft periscopic sextant
2127807 Indicating Instrument, V.E. Carbonara (Bendix Aviation Co), Aug 23 1938, 116/287; 33/348; 116/299; 359/440 -
2132286 Change Responsive Controlling Means, V.E. Carbonara (Bendix Aviation Corp), Oct 4 1938, 73/386; 73/178.00R; 415/13 - clockwork on elevation axis
Cited Patent Filing date Publication date Applicant Title US2369622 * Jun 11, 1941 Feb 13, 1945 Toulon Pierre Maric Gabriel Orientation system US2462925 * Dec 7, 1946 Mar 1, 1949 Sperry Corp Radiant energy directional apparatus NL33746C *
Title not availableReferenced by
Citing Patent Filing date Publication date Applicant Title US3127516 * May 16, 1960 Mar 31, 1964 Singer Inc H R B Star tracker having adjustable scan dependent upon radiation intensity US3147381 * Jun 30, 1961 Sep 1, 1964 Barnes Eng Co Two color radiometer for distinguishing radiations from sources at dieferent temperatures US3177362 * Oct 2, 1961 Apr 6, 1965 Lockheed Aircraft Corp Infrared tracker US3242343 * Dec 11, 1961 Mar 22, 1966 Kollsman Instr Corp Oscillating reed scanner with two excursions and aperture with central opaque region US3274393 * Oct 10, 1962 Sep 20, 1966 Kollsman Instr Corp Single modulation star tracker US3454776 * May 19, 1965 Jul 8, 1969 Leitz Ernst Gmbh Method and apparatus for determining the positions of indicia utilizing an oscillating light beam and detecting an odd harmonic in the output
Cited Patent Filing date Publication date Applicant Title US2961545 * Oct 23, 1959 Nov 22, 1960 Barnes Eng Co Tracker for moving objects US3012148 * Jul 2, 1951 Dec 5, 1961 Franklin Hummer Robert Infrared tracker US3080485 * Jun 22, 1960 Mar 5, 1963 Singer Inc H R B Stellar orientation monitoring system US3138712 * Aug 5, 1959 Jun 23, 1964 Bunker Ramo Photosensitive energy detection system
1299459 Panoramic range-finder, Graves Griffith, Apr 8, 1919, 356/16, 359/401 - keeps image right side up while panning horizon. uses Amici roof prism (Wiki)
When a telescope has a mirror at the objective end that mirror is rotated about an axis going through the centerline of the telescope, the image seen through the telescope also rotates. So, if the telescope was pointed up and the mirror was at 45 degrees to the telescope centerline, the horizon could be scanned, but only at one azimuth angle would the ground be at the bottom of the image. At an azimuth 180 degrees from there the image would be upside down. So for panoramic range-finders, panoramic telescopes, periscopes and sextants with panoramic capability something needs to be done to keep the image erect.
If the schematic of the star tracker can be located or reverse engineered, then it may be possible to use the star tracker without all the other boxes in the system directly from a PC and using a custom made interface.
Synchro Systems -
Control Sciences Inc. -
Analog Devices - Synchro to Digital Converters -
ILC Data Device Corporation -
Natel Engineering/Muirhead hybrid contract manufacturer, but has Synchro history
Pentland Systems - VME synchro converters
Computer Conversions Corp. - amplifiers -
VMIC - synchro converters - Tutorial -
Poly-Scientific -Resolvers & Synchros - Synchro Application Data -
Hotek - North Atlantic Angle Position Indicator, API Model 8810 -
Micro-Precision Technologies - Synchro- and Resolver-to-Digital, Digital-to-Synchro and -Resolver -
BBG Inc. - serial converter -
ICPE S.A - Synchros & Resolvers
Integrated Publishing- Gunners Mate Training Chapt 5 -Synchro Circuits -
North Atlantic Industries -
FT Technologies Ltd - Synchro/Resolver Converters -
Science Engineering Associates, Inc. - Synchro Digital Converter for INS Interfaces -
KineticSystems Company, LLC - 3-channel, Digital-to-synchro Converter -
ACTIS Computer - RDC-20 Dual-channel Resolver / Synchro Converter -
Eagle Technology - PC-40 4 Channel Digital to Synchro Converter ISA Board -
- Multi Mission Military Aircraft Simulator -
North Atlantic Instruments - angle position indicators and realted equipment for synchro/resolvers, S/R simulator with 3VA output. 76CS1 will measure 8 chan & drive 6 chan with 1.2VA.
Test Set Synchro Type TTU-23/E -
There is also a program for the Palm Pilot called "astro compass". This uses the time and location of an observer to calculate some astronomical data.
Lt. Bill Brandt went missing on 20 Feb 1955 while on a test flight of a "Kollsman photoelectric sextant". The aircraft took off from Turner Air Force Base in Georgia (not that far from the Atlantic ocean).
2713134 Radiant Energy Controlled Follow-up System, Kollsman, App: Pub: July 12, 1955 - photo multiplier and 400 Hz rotating mask, automatic star follower - may be the photoelectric sextant being tested in the new F-84 application?
The following patents contain "photoelectric sextant" (as far as Google Optical Character Recognition knows).2941082 Photoelectric automatic sextant, Victor E Carbonara, Howard J Eckweiler, Louis E Sharpe, Kollsman Instrument Corp, App: App: 1956-01-23 -
this may be the star tracker for the Hound Dog Missile (Wiki) and might be a better fit to the F-84 than the MD-1 which is much much larger.2947872 Star tracking system, Victor E Carbonara, Howard J Eckweiler, James B O'maley, Paul D Hansell, Kollsman Instrument Corp, App:1956-01-23 - this is the basic theory about how the search disk ends up driving the Az-El motors.
"The first air-drop test of a dummy Hound Dog was carried out in November 1958" - Would the star tracker for the Hound Dog be ready for a test flight in 1955?
"The Hound Dog missile's development was completed in only 30 months (2 years & 6 months)", so November - 6 mo = May, 1958 - 2 years = 1956, so Hound Dog development started May 1956, i.e. after the F-84 went missing.
-------------- the above patents may be related, but the below patents are probably too new --------------
2998529 Automatic astrocompass, David B Nichinson, James J Connors, Kollsman Instrument Corp, App; 1958-06-19 - This is the MD-1 and it's necessary vertical gyro.
3042296 Celestial data computer, Victor E Carbonara, Mac-Donald E Douglas, Kollsman Instrument Corp, App: 1958-06-19 - the MD-1 mechanical computer (technology similar to the Torpedo Data Computer).
Stellar Time Keeping -
Astro-Compass MkII - no optics, just open gun sights and angle scales.
Sextant, Aircraft, Periscopic - Optics, clockwork integrator
Surveying - Theodolites - Pibal theodolites (easy to use when looking up) -
Kollsman later provided an Astro-Compass System (a combination mechanical, electro-mechanical and electronic analog computer system).BOMB/NAV - Guestbook & War Stories - people who worked on these.
This Astro-Compass System solved the celestial navigation problem by locking unto light from the sun in daylight hours, and to the intensity of light from stars in the darkness of night. Its gyro system was so sensitive, bench systems had to be installed on concrete pedestals several feet deep into the ground, to minimize disturbance from earth vibrations by the roll of 18-wheeler trucks riding highways ten miles away.
This Astro-Compass System was installed only in E and F model B-52s, and later removed. (I have no proof, but, from experience, one of the reasons for removal could have come from this system's ability to lock-on to the glow from lightning bugs impacted on the glass dome during B-52 take-off rolls, later blocking points of view, rendering the system inoperative in-flight.)
Atop the stabilization unit, and protruding slightly above the skin of the fuselage, is the rounded cupola of the star tracker unit. By setting on his astro control panel the Greenwich Hour Angle, the sidereal hour angle, and the declination of the sun or star to be used for navigational purposes, the navigator can cause the astro tracker to lock onto the heavenly body, after which it will provide continuous heading information to the computer.B-52 Stratofortress Association -
The N5G Hound dog missle also used the astro tracker.
Yankee Air Museum - has restored B-52D but no MD-1 infoThe Book: The Praetorian STARShip: The Untold Story of the Combat Talon - mentions the use of the MD-1 in relation to the Terrain Avoidance/Terrain Following RADAR
Kollsman - still in business making similar products
B-52 Stratofortress Association -
Air University at Maxwell AFB -
Purchased from Omaha's - ASTRO TRACKER,B-52D
"The ground and inflight operating procedures are extremely simple. The ground preparation of the equipment is accomplished in the following manner. Turn the power switch on and wait two minutes. Using a master watch or WWV time hack set and start the clock. Select the proper mode of operation (Sidereal or Solar) for the type of body to be tracked. Set up the proper GHA of the sun or aries from the air almanac. The GHA selected should agree with the time on the clock. Set the SHA as determined from the Air Almanac. For sun or planet tracking the SHA is set at zero.The Navigator Vol 7 No. 2 May 1961 " Keep it Automatic" Maj. Stuart E. Burtt, - " It might prove advantageous to develop a small, inexpensive, hand-held integrator to facilitate the use of theMD-1".
When selecting a star try to select a low rising or high setting body to provide maximum continuous tracking time. Also try to choose a star forward of the aircraft. Star tracking should be limited to stars between six and sixty degrees in altitude. Set declination of the body from the air almanac. The latitude and longitude information may be set manually in counters provided or taken automatically from the Bomb-Navsystem. The latter is by far the most desirable. The equipment is now ready to use in-flight for celestial heading reference, azimuth, and altitude intercept information."
Computer altitude azimuth
Automatic Astro Compass Type MD-1
Stock No. 6605-673-6737
Serial No. AF60-972
Mfrs Part No. A26960 00 002
Contract No. AF3316001-41563
Kollsman Instrument Corporation
page created Oct 2001.