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System Sensor L-Series horn/strobe at Wawa in Abingdon, Maryland.
Ben Schumin is a professional photographer who captures the intricacies of daily life. This image is all rights reserved. Contact me directly for licensing information.
current ATMs will see a new design adopting a fingerprint biometric sensor by pressing yr thumb onto the sensor.....www.scientificamerican.com
+++ DISCLAIMER +++
Nothing you see here is real, even though the conversion or the presented background story might be based on historical facts. BEWARE!
Some background:
The Grumman Mohawk began as a joint Army-Marine program through the then-Navy Bureau of Aeronautics (BuAer), for an observation/attack plane that would outperform the light and vulnerable Cessna L-19 Bird Dog. In June 1956, the Army issued Type Specification TS145, which called for the development and procurement of a two-seat, twin turboprop aircraft designed to operate from small, unimproved fields under all weather conditions. It would be faster, with greater firepower, and heavier armor than the Bird Dog, which had proved very vulnerable during the Korean War.
The Mohawk's mission would include observation, artillery spotting, air control, emergency resupply, naval target spotting, liaison, and radiological monitoring. The Navy specified that the aircraft had to be capable of operating from small "jeep" escort class carriers (CVEs). The DoD selected Grumman Aircraft Corporation's G-134 design as the winner of the competition in 1957. Marine requirements contributed an unusual feature to the design: since the Marines were authorized to operate fixed-wing aircraft in the close air support (CAS) role, the mockup featured underwing pylons for rockets, bombs, and other stores, and this caused a lot of discord. The Air Force did not like the armament capability of the Mohawk and tried to get it removed. On the other side, the Marines did not want the sophisticated sensors the Army wanted, so when their Navy sponsors opted to buy a fleet oil tanker, they eventually dropped from the program altogether. The Army continued with armed Mohawks (and the resulting competence controversy with the Air Force) and also developed cargo pods that could be dropped from underwing hard points to resupply troops in emergencies.
In mid-1961, the first Mohawks to serve with U.S. forces overseas were delivered to the 7th Army at Sandhofen Airfield near Mannheim, Germany. Before its formal acceptance, the camera-carrying AO-1AF was flown on a tour of 29 European airfields to display it to the U.S. Army field commanders and potential European customers. In addition to their Vietnam and European service, SLAR-equipped Mohawks began operational missions in 1963 patrolling the Korean Demilitarized Zone.
Germany and France showed early interest in the Mohawk, and two OV-1s were field-tested by both nations over the course of several months. No direct orders resulted, though, but the German Bundesheer (Army) was impressed by the type’s performance and its capability as an observation and reconnaissance platform. Grumman even signed a license production agreement with the French manufacturer Breguet Aviation in exchange for American rights to the Atlantic maritime patrol aircraft, but no production orders followed.
This could have been the end of the OV-1 in Europe, but in 1977 the German government, primarily the interior ministry and its intelligence agency, the Bundesnachrichtendienst (BND), showed interest in a light and agile SIGINT/ELINT platform that could fly surveillance missions along the inner-German border to the GDR and also to Czechoslovakia. Beyond visual reconnaissance with cameras and IR sensors, the aircraft was to be specifically able to identify and locate secret radio stations that were frequently operated by Eastern Block agents (esp. by the GDR) all across Western Germany, but primarily close to the inner-German border due to the clandestine stations’ low power. The Bundeswehr already operated a small ELINT/ECM fleet, consisting of converted HFB 320 ‘Hansa’ business jets, but these were not suited for stealthy and inconspicuous low flight level missions that were envisioned, and they also lacked the ability to fly slowly enough to locate potential “radio nests”.
The pan and the objective were clear, but the ELINT project caused a long and severe political debate concerning the operator of such an aerial platform. Initially, the Bundesheer, who had already tested the OV-1, claimed responsibility, but the interior ministry in the form of the German customs department as well as the German police’s Federal Border Guard, the Bundesgrenzschutz and the Luftwaffe (the proper operator for fixed-wing aircraft within the German armed forces), wrestled for this competence. Internally, the debate and the project ran under the handle “Schimmelreiter” (literally “The Rider on the White Horse”), after a northern German legendary figure, which eventually became the ELINT system’s semi-official name after it had been revealed to the public. After much tossing, in 1979 the decision was made to procure five refurbished U.S. Army OV-1As, tailored to the German needs and – after long internal debates – operate them by the Luftwaffe.
The former American aircraft were hybrids: they still had the OV-1A’s original short wings, but already the OV-1D’s stronger engines and its internal pallet system for interchangeable electronics. The machines received the designation OV-1G (for Germany) and were delivered in early 1980 via ship without any sensors or cameras. These were of Western German origin, developed and fitted locally, tailored to the special border surveillance needs.
The installation and testing of the “Schimmelreiter” ELINT suite lasted until 1982. It was based on a Raytheon TI Systems emitter locator system, but it was locally adapted by AEG-Telefunken to the airframe and the Bundeswehr’s special tasks and needs. The system’s hardware was stowed in the fuselage, its sensor arrays were mounted into a pair of underwing nacelles, which occupied the OV-1’s standard hardpoints, allowing a full 360° coverage. In order to cool the electronics suite and regulate the climate in the internal equipment bays, the OV-1G received a powerful heat exchanger, mounted under a wedge-shaped fairing on the spine in front of the tail – the most obvious difference of this type from its American brethren. The exact specifications of the “Schimmelreiter” ELINT suite remained classified, but special emphasis was placed upon COMINT (Communications Intelligence), a sub-category of signals intelligence that engages in dealing with messages or voice information derived from the interception of foreign communications. Even though the “Schimmelreiter” suite was the OV-1Gs’ primary reconnaissance tool, the whole system could be quickly de-installed for other sensor packs and reconnaissance tasks (even though this never happened), or augmented by single modules, what made upgrades and mission specialization easy. Beyond the ELINT suite, the OV-1G could be outfitted with cameras and other sensors on exchangeable pallets in the fuselage, too. This typically included a panoramic camera in a wedge-shaped ventral fairing, which would visually document the emitter sensors’ recordings.
A special feature of the German OV-1s was the integration of a brand new, NATO-compatible “Link-16” data link system via a MIDS-LVT (Multifunctional Information Distribution System). Even though this later became a standard for military systems, the OV-1G broke the ground for this innovative technology. The MIDS was an advanced command, control, communications, computing and intelligence (C4I) system incorporating high-capacity, jam-resistant, digital communication links for exchange of near real-time tactical information, including both data and voice, among air, ground, and sea elements. Outwardly, the MIDS was only recognizable through a shallow antenna blister behind the cockpit.
Even though the OV-1Gs initially retained their former American uniform olive drab livery upon delivery and outfitting in German service, they soon received a new wraparound camouflage for their dedicated low-level role in green and black (Luftwaffe Norm 83 standard), which was better suited for the European theatre of operations. In Luftwaffe service, the OV-1Gs received the tactical codes 18+01-05 and the small fleet was allocated to the Aufklärungsgeschwader (AG) 51 “Immelmann”, where the machines formed, beyond two squadrons with RF-4E Phantom IIs, an independent 3rd squadron. This small unit was from the start based as a detachment at Lechfeld, located in Bavaria/Southern Germany, instead of AG 51’s home airbase Bremgarten in South-Western Germany, because Lechfeld was closer to the type’s typical theatre of operations along Western Germany’s Eastern borders. Another factor in favor of this different airbase was the fact that Lechfeld was, beyond Tornado IDS fighter bombers, also the home of the Luftwaffe’s seven HFB 320M ECM aircraft, operated by the JaBoG32’s 3rd squadron, so that the local maintenance crews were familiar with complex electronics and aircraft systems, and the base’s security level was appropriate, too.
With the end of the Cold War in 1990, the OV-1Gs role and field of operation gradually shifted further eastwards. With the inner-German Iron Curtain gone, the machines were now frequently operated along the Polish and Czech Republic border, as well as in international airspace over the Baltic Sea, monitoring the radar activities along the coastlines and esp. the activities of Russian Navy ships that operated from Kaliningrad and Saint Petersburg. For these missions, the machines were frequently deployed to the “new” air bases Laage and Holzdorf in Eastern Germany.
In American service, the OV-1s were retired from Europe in 1992 and from operational U.S. Army service in 1996. In Germany, the OV-1 was kept in service for a considerably longer time – with little problems, since the OV-1 airframes had relatively few flying hours on their clocks. The Luftwaffe’s service level for the aircraft was high and spare parts remained easy to obtain from the USA, and there were still OV-1 parts in USAF storage in Western German bases.
The German HFB 320M fleet was retired between 1993 and 1994 and, in part, replaced by the Tornado ECR. At the same time AG 51 was dissolved and the OV-1Gs were nominally re-allocated to JaboG 32/3. With this unit the OV-1Gs remained operational until 2010, undergoing constant updates and equipment changes. For instance, the machines received in 1995 a powerful FLIR sensor in a small turret in the aircraft’s nose, which improved the aircraft’s all-weather reconnaissance capabilities and was intended to spot hidden radio posts even under all-weather/night conditions, once their signal was recognized and located. The aircrafts’ radio emitter locator system was updated several times, too, and, as a passive defensive measure against heat-guided air-to-air missiles/MANPADS, an IR jammer was added, extending the fuselage beyond the tail. These machines received the suffix “Phase II”, even though all five aircraft were updated the same way.
Reports that the OV-1Gs were furthermore retrofitted with the avionics to mount and launch AIM-9 Sidewinder AAMs under the wing tips for self-defense remained unconfirmed, even more so because no aircraft was ever seen carrying arms – neither the AIM-9 nor anything else. Plans to make the OV-1Gs capable of carrying the Luftwaffe’s AGM-65 Maverick never went beyond the drawing board, either. However, BOZ chaff/flare dispenser pods and Cerberus ECM pods were occasionally seen on the ventral pylons from 1998 onwards.
No OV-1G was lost during the type’s career in Luftwaffe service, and after the end of the airframes’ service life, all five German OV-1Gs were scrapped in 2011. There was, due to worsening budget restraints, no direct successor, even though the maritime surveillance duties were taken over by Dornier Do 228/NGs operated by the German Marineflieger (naval air arm).
General characteristics:
Crew: Two: pilot, observer/systems operator
Length: 44 ft 4 in (13.53 m) overall with FLIR sensor and IR jammer
Wingspan: 42 ft 0 in (12.8 m)
Height: 12 ft 8 in (3.86 m)
Wing area: 330 sq. ft (30.65 m²)
Empty weight: 12,054 lb (5,467 kg)
Loaded weight: 15,544 lb (7,051 kg)
Max. takeoff weight: 18,109 lb (8,214 kg)
Powerplant:
2× Lycoming T53-L-701 turboprops, 1,400 shp (1,044 kW) each
Performance:
Never exceed speed: 450 mph (390 knots, 724 km/h)
Maximum speed: 305 mph (265 knots, 491 km/h) at 10,000 ft (3,050 m)
Cruise speed: 207 mph (180 knots, 334 km/h) (econ cruise)
Stall speed: 84 mph (73 knots, 135 km/h)
Range: 944 mi (820 nmi, 1,520 km) (SLAR mission)
Service ceiling: 25,000 ft (7,620 m)
Rate of climb: 3,450 ft/min (17.5 m/s)
Armament:
A total of eight external hardpoints (two ventral, three under each outer wing)
for external loads; the wing hardpoints were typically occupied with ELINT sensor pods, while the
ventral hardpoints frequently carried 300 l drop tanks to extend loiter time and range;
Typically, no offensive armament was carried, even though bombs or gun/missile pods were possible.
The kit and its assembly:
This build became a submission to the “Reconnaissance” Group Build at whatifmodellers.com in July 2021, and it spins further real-world events. Germany actually tested two OV-1s in the Sixties (by the German Army/Bundesheer, not by the air force), but the type was not procured or operated. The test aircraft carried a glossy, olive drab livery (US standard, I think) with German national markings.
However, having a vintage Hasegawa OV-1A in the stash, I wondered what an operational German OV-1 might have looked like, especially if it had been operated into the Eighties and beyond, in the contemporary Norm 83 paint scheme? This led to this purely fictional OV-1G.
The kit was mostly built OOB, and the building experience was rather so-so – after all, it’s a pretty old mold/boxing (in my case the Hasegawa/Hales kit is from 1978, the mold is from 1968!). Just a few things were modified/added in order to tweak the standard, short-winged OV-1A into something more modern and sophisticated.
When searching for a solution to mount some ELINT sensor arrays, I did not want to copy the OV-1B’s characteristic offset, ventral SLAR fairing. I rather settled for the late RV-1D’s solution with sensor pods under the outer wings. Unfortunately, the OV-1A kit came with the type’s original short wings, so that the pods had to occupy the inner underwing pair of hardpoints. The pods were scratched from square styrene profiles and putty, so that they received a unique look. The Mohawk’s pair of ventral hardpoints were mounted, but – after considering some drop tanks or an ECM pod there - left empty, so that the field of view for the ventral panoramic camera would not be obscured.
Other small additions are some radar warning sensor bumps on the nose, some extra antennae, a shallow bulge for the MIDS antenna on the spine, the FLIR turret on the nose (with parts from an Italeri AH-1 and a Kangnam Yak-38!), and I added a tail stinger for a retrofitted (scratched) IR decoy device, inspired by the American AN/ALG-147. This once was a Matchbox SNEB unguided missile pod.
Painting and markings:
For the intended era, the German Norm 83 paint scheme, which is still in use today on several Luftwaffe types like the Transall, PAH-2 or CH-53, appeared like a natural choice. It’s a tri-color wraparound scheme, consisting of RAL 6003 (Olivgrün), FS 34097 (Forest Green) and RAL 7021 (Teerschwarz). The paints I used are Humbrol 86 (which is supposed to be a WWI version of RAL 6003, it lacks IMHO yellow but has good contrast to the other tones), Humbrol 116 and Revell 9. The pattern itself was adapted from the German Luftwaffe’s Dornier Do 28D “Skyservants” with Norm 83 camouflage, because of the type’s similar outlines.
A black ink washing was applied for light weathering, plus some post-shading of panels with lighter shades of the basic camouflage tones for a more plastic look. The cockpit interior was painted in light grey (Humbrol 167), while the landing gear and the interior of the air brakes became white. The scratched SLAR pods became light grey, with flat di-electric panels in medium grey (created with decal material).
The cockpit interior was painted in a rather light grey (Humbrol 167), the pilots received typical olive drab Luftwaffe overalls, one with a white “bone dome” and the other with a more modern light grey helmet.
The decals were improvised. National markings and tactical codes came from TL Modellbau sheets, the AG 51 emblems were taken from a Hasegawa RF-4E sheet. The black walkways were taken from the Mohak’s OOB sheet, the black de-icer leading edges on wings and tail were created with generic black decal material. Finally, the model was sealed with a coat of matt acrylic varnish (Italeri).
An interesting result, and the hybrid paint scheme with the additional desert camouflage really makes the aircraft an unusual sight, adding to its credibility.
A close-up view of the light sensor employed by the phase detection autofocus system in the DSLR camera I took apart after its shutter failed. The horizontal and vertical rows of dark rectangles are the light-sensitive elements. Horizontal rows detect vertical edges in the scene, and vertical rows detect horizontal edges.
The 5 mm scale bar drawn at the bottom of the frame shows the size of the sensor chip. The resolution of the 4k version of this photo is about 3 µm per pixel.
Manufactured by Agfa Kamerawerk AG, Munich, West Germany
Model: c.1970, (all models of Silette produced between 1953-1974)
Agfa logo on the front of the camera: black relief
35 mm film Viewfinder camera
Lens:Agfa Color - Agnar 45mm f/2.8
Aperture: f/2.8 -f /22 , stepless allowing for easy adjustment with the TTL meter
setting: ring and scale on the back of the lens
Focusing: front ring manual focus, w/ DOF scale
Focus range: 1-5m +inf.
Shutter: Parator speeds: 30, 60, 125, 300 +B, extremely quiet
setting : ring and scale on the lens
Shutter release: Red "Sensor" shutter release button,
very smooth and sensitive so no camera shake
Cable release socket: on the back of the top plate
Exposure meter: TTL (coupled to the lens) Selenium Optima 200 Sensor (working !.)
Exposure setting: via 1- the small needle window on the top plate, 2- the indicator in the viewfinder, set the speed and turn the aperture ring
Film speed range: ASA 25-400 (DIN 15-27), setting knob and scales on the lens
View finder: bright frame finder,
Cocking lever: also winds the film, short stroke, on the left of the bottom plate
Frame counter: advance type, manual reset by a button behind the counter window, on the bottom plate
Re-wind release and re-winding: the black lever marked R and arrow on the right lower side of the lens releases and engages the reversing gear
thus the cocking and winding lever is the re-wind lever now
Flash PC socket: none, you can use a flash sync. cord with an Agfa flash adapter
Hot-shoe: flash sync. bulbs 1/30, electronic all speeds
Self-timer: none
Back cover: hinged, opens by a latch on the right side of the camera
Film loading: special easy quick loading system
Body: metal
Tripod socket: 1/4''
serial no. LW 6837 BC
The Silette series' rangefinder models were called Super Silette. There was also an interchangeable lens rangefinder model called the Ambi Silette.
APS-C sensor, X-Trans CMOS III.
Flagship model of Fuji X series. My husband wrote the review in Japanese, I took the photos of the camera, in March.
The first part
news.mynavi.jp/articles/2016/03/09/x-pro2_1/
The latter part
Manufactured by Agfa Kamerawerk AG, Munich, West Germany
Model: c.1970, (all models of Silette produced between 1953-1974)
Agfa logo on the front of the camera: black relief
35 mm film Viewfinder camera
Lens:Agfa Color - Agnar 45mm f/2.8
Aperture: f/2.8 -f /22 , stepless allowing for easy adjustment with the TTL meter
setting: ring and scale on the back of the lens
Focusing: front ring manual focus, w/ DOF scale
Focus range: 1-5m +inf.
Shutter: Parator speeds: 30, 60, 125, 300 +B, extremely quiet
setting : ring and scale on the lens
Shutter release: Red "Sensor" shutter release button,
very smooth and sensitive so no camera shake
Cable release socket: on the back of the top plate
Exposure meter: TTL (coupled to the lens) Selenium Optima 200 Sensor (working !.)
Exposure setting: via 1- the small needle window on the top plate, 2- the indicator in the viewfinder, set the speed and turn the aperture ring
Film speed range: ASA 25-400 (DIN 15-27), setting knob and scales on the lens
View finder: bright frame finder,
Cocking lever: also winds the film, short stroke, on the left of the bottom plate
Frame counter: advance type, manual reset by a button behind the counter window, on the bottom plate
Re-wind release and re-winding: the black lever marked R and arrow on the right lower side of the lens releases and engages the reversing gear
thus the cocking and winding lever is the re-wind lever now
Flash PC socket: none, you can use a flash sync. cord with an Agfa flash adapter
Hot-shoe: flash sync. bulbs 1/30, electronic all speeds
Self-timer: none
Back cover: hinged, opens by a latch on the right side of the camera
Film loading: special easy quick loading system
Body: metal
Tripod socket: 1/4''
serial no. LW 6837 BC
The Silette series' rangefinder models were called Super Silette. There was also an interchangeable lens rangefinder model called the Ambi Silette.
This is a 5 megapixel image sensor from my old HTC Aria Smart Phone.
This is a little bigger than 1:1 macro since the Nikkor 40mm 2.8G DX can be manually focused a little past 1:1. I used both of my SB-700's for this. They were set to 1/50th power.
digital camera sensor size chart.
inspired by rising buzz about micro four thirds, which is just what i was missing so long. it was made first for myself, as long, as other charts, just to make an system in all absorbed information. maybe someone of you will find it useful.
Lorenzo Moggio cleaning sensors as part of his regular maintenance for scientific instruments.
During summer aircraft take off on an almost daily basis. Concordia is a hubbub of activity as researchers from disciplines as diverse as astronomy, seismology, human physiology and glaciology descend to work in this unique location.
For the rest of the year, around 14 crewmembers remain to keep the station running during the cold, dark winter months.
ESA sponsors a research medical doctor in Concordia to study the effects of living in isolation. The extreme cold, sensory deprivation and remoteness make living in Concordia similar to living on another planet.
Credits: ESA/IPEV/PNRA-B. Healey
D300 + af200 mm + ais 35 mm reverse.
SB-29-s flash.
40 pictures @ 5 um zerene stacking.
I found the sensor type number on the chip:
Image sensor CCD KC73129
• Number of Total Pixels: 537(H) ´ 597(V)
• Number of Effective Pixels: 500(H) ´ 582(V)
• Chip Size: 6.00mm(H) ´ 5.10mm(V)
• Unit Pixel Size: 9.80um(H) ´ 6.30um(V)
100% crop image on the corner.
This small sensor has a decent range and can easily cover the distance of a room and works really well even in the dark. The other feature I really like about this particular sensor is the ability to set the delay on how frequently it can be triggered. Anywhere from 4 seconds up to 2 hours. I'll probably set it somewhere in the range of 10-15 seconds.
PNNL’s improved Sensor Fish is a small tubular device filled with sensors that analyze the physical stresses fish experience as they pass through dams and other hydropower structures. The device’s latest version costs about 80 percent less and can be used in more hydro structures than its predecessor, according to a paper published in the journal Review of Scientific Instruments.
Terms of Use: Our images are freely and publicly available for use with the credit line, "Courtesy of Pacific Northwest National Laboratory." Please use provided caption information for use in appropriate context.
sensor size
Full Frame
APS-H
APS-C
Micro 4/3rds
Black Magic Cinema Camera
Digital Bolex
Super 16mm Film
16mm Film
Digital Bolex @ 2K
Ikonoskop &
Digital Bolex FullHD
and the image circle of the S16 Optar Illuminas
8mm,
9.5mm,
12mm,
16mm,
25mm,
50mm
Olympus E-500 ( KODAK CCD sensor ) + Olympus Zuiko Digital ED 50mm f/2.0 Macro
OLYMPUS DIGITAL CAMERA
Here is an older picture, as I am without my 5d at the moment.
Working on the Heidelberg exposed Set, revealed how desperate my MkII was in need of some serious sensor cleaning (Thx Russ). After weeping over messed up shots, I brought the cam in and will be able to pick it up on Tuesday.
It feels weird not having my Cam, like something is missing.
The sensors detect the level of pellets and email operator when to order more fuel.
Oakridge Elementary Biomass Heat System. Fuel: wood pellets
Oakridge, OR
"these two modes of invisibility - that which is hidden behind the things that we see, and that which is hidden inside the things we see - lend a pervasive sense of enigma, and unknowableness, to the everyday world of our direct experience. a sense that we are in continual, felt relationship with the unseen. it is a sensation that readily dissipates, however, when we abstractly ponder this earthly world as though we were not entirely a part of it, considering nature with the cool detachment of an engineer gazing at his blueprints on the wall, or that of a spectator watching a satellite image of the earth projected on the flat screen of her computer. however, as soon as we return to the immediacy of the present moment, and hence to our ongoing, animal experience in the midst of this sensorial world, then the flatness dissolves, and the enigmatic depth of the world becomes apparent."
~david abram, from "the invisibles," an essay in the spring 2006 issue of parabola magazine: "coming to our senses"
dear friends, let us meet in this moment...
may all travelers find joy!!
jeanne
altered digital image, february 10, 2009
(a cameraphone photo taken while walking in an interior garden the other day)
Agfa Optima Sensor compact 35mm camera. Top plate showing rewind button, depressed and turned to use the advance lever to rewind the film.
Specifications:-
Type: 35mm compact camera
Size: 104 mm x 68 mm x 54 mm (W x H x D)
Image Format: 24 x 36 mm (W x H)
Lens: Agfa Solitar, 40 mm f/2.8
Diaphragm: Automatic f/2.8 to f/22
Focusing: Manual scale pictograms on top of the focus ring/ meter/feet scale on bottom, focusing 3ft/1.09m - infinity
Shutter Speeds: 1/500 second - 15 seconds
Viewfinder: Large direct finder with parallax marks for near focus
Film Loading: Manual
Film Transport: Manual single stroke lever, also used to rewind film when the 'R' button is depressed and turned
Film Speeds: 25 ASA/15 DIN to 500 ASA/28 DIN, selected on a ring around the lens
Flash Contact: Hot shoe, aperture selected manually with flash
Cable Release Socket: On left hand side of the camera body
Tripod Socket: 1/4 in. on right hand side which doubles as camera strap attachment
Battery: 3 V625U batteries, located by opening the camera back
Balloon with cornflour inside popped with a dart. Shutter open, SB900 front, camera right, at 1/128 triggered by Triggertrap on sound sensor.
The nDETECT sensors undergo testing at Sandia. Money from DOE’s Energy I-Corps program will help the technology advance toward commercialization.
Learn more at bit.ly/3TqfJHw
Photo by Craig Fritz
Has two spots on the lower left that won't blow off. You can see the shadow of one of them through the low pass filter
Sensor's been cleaned up by Nikon School on January. This is a picture of the empty blue sky in June.
Camera is currently being fixed at Nikon's, I hope this will be its last trip.
Medtronic Continuous Glucose Monitoring
Update: I am now, as of October 2017, using the Guardian Sensors with the 760G insulin pump. Same look different tech. Not a fan, as of December, as the sensors are supposed to last 7 days. Mine quit on day 6.
Agfa Silette LK Sensor, introduced 1970, perhaps one of the last Silettes and an early Agfa with the red shutter release button. The body is based on the Agfa Optima 200 from 1968.
It is a low-budget camera, the lens barrel and the housing are made of plastic, though the top and the bottom look like metal. This camera hasn't a rewind crank, the rewinding is done by the advance lever, when the button "R" is tripped before, so the inner mechanism is complex.
The lens is a Color-Agnar 2.8/45 mm with three elements, the shutter is a Parator with 1/30 to 1/300 s and B. The Selenium exposure meter is coupled and the match needle is displayed in the viewfinder and on top, the ASA range is from 25 to 400 ASA. All settings has to be done manually, like on all Silettes, I think. The LK has a thread for a cable release on the backside and a hot shoe. There is no self-timer, no focussing aid and the frame counter has to be reset manually.
(If you want to remove the top plate: there is a third screw hidden in the hot shoe. The cover in the hot shoe has the most diabolic clip mechanism I've ever experienced.)
Principal investigator Jacques Loui, left, and a firmware developer are part of a team redesigning high-performance radar as a flexible, multipurpose sensor.
Researchers are working to replace legacy analog radars commonly used by the military with a new, digital, software-defined system called Multi-Mission Radio Frequency Architecture. The overhauled design promises U.S. warfighters unprecedented flexibility and performance during intelligence, surveillance and reconnaissance operations, even against sophisticated adversaries.
Learn more at bit.ly/3hKHWM7
Photo by Craig Fritz.