View allAll Photos Tagged generaldynamics
F-111F. C.N. 12. 492nd TFS at RAF Lakenheath. Withdrawn from service to AMARC 18 October 1995 as AA FV0213. Scrapped in June 2012. Photo Credit's: Unknown to me (Kodachrome Slide dated August 1980)
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
PictionID:54636977 - Catalog:14_035152 - Title:Atlas Centaur Testing Details: Ejection Post Test; Centaur Insulation Panels Date: 01/08/1964 - Filename:14_035152.tif - - ---- Images from the Convair/General Dynamics Astronautics Atlas Negative Collection. The processing, cataloging and digitization of these images has been made possible by a generous National Historical Publications and Records grant from the National Archives and Records Administration---Please Tag these images so that the information can be permanently stored with the digital file.---Repository: San Diego Air and Space Museum
F-111E. C.N. E-230. 55th FS from RAF Upper Heyford. Photo taken at Florennes Air Base, Belgium, 27 August, 1993. Withdrawn from service to AMARC 8 December, 1993 as AA FV0198. Departed AMARC 11 January, 2012 to HVF West Yard (scrapped probably in June 2012). Photo Credit's: Unknown to me (Reprint Scan)
F-111E. C.N. E-234. 77th TFS at RAF Upper Heyford. Last flew with the 55th TFS. Withdrawn from service to AMARC 28 October, 1993 as AA FV0187. Departed AMARC to HVF West Yard 11 January, 2012 (Scrapped) Photo Credit's: Unknown to me (original photo printed on rough paper that doesn't scan well). Judging by the dry grass, I'd bet this was taken around Summer 1976.
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
General Dynamics F-16AM Fighting Falcon
"Dream Viper" Solo Display
Belgische Luftwaffe / Belgian Air Force
ZigAirMeet 2023, Mollis, Schweiz
Belgian Air Component (formerly Belgian Air Force, or Belgische Luchtmacht / Force aérienne belge) F-16A FA-56.
Online sources indicate that it has received an update and service-life extension, and is now designated F-16AM.
According to Joe Baugher's serial number database, this aircraft was procured under USAF s/n 80-3547, and assembled by SABCA for the Belgian Air Force.*
Red Flag 19-2
Nellis Air Force Base
Las Vegas, Nevada
*References:
General Dynamics F-16D-30-CF "Fighting Falcon" 87-0377 (ED)
416th Flight Test Squadron, Edwards Air Force Base, California.
Pass through Star Wars Canyon, Red Flag 19-1
www.flickr.com/photos/yesiwood/47093727451/in/album-72157...
87-0377
ED
F-16D-30-CF
5D-71
416th FLTS
Active
Jun 2007
Oct 2020
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
Dr. Alan M. Lovelace served as NASA's Deputy Administrator from July 2, 1976 to July 10, 1981. After graduating with a Doctor of Philosophy Degree in Organic Chemistry in 1954, Dr. Lovelace went to work for the United States Air Force and served in many scientific research positions until he left to join NASA as Associate Administrator of the Office of Aeronautics and Space Technology. In 1976 he became NASA's Deputy Administrator and served until he retired in 1981. After retirement Dr. Lovelace worked for the General Dynamics Corporation.
Credit: NASA
Image Number: Lovelace01
Date: Circa 1976
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977..
Repository: San Diego Air and Space Museum Archive
PictionID:43057564 - Catalog:14_003943 - Title:Atlas 113D-Mercury Details: MA-8; Alert; Pad 14 09/08/1962 - Filename:14_003943.TIF - - - - Image from the Convair/General Dynamics Astronautics Atlas Negative Collection---Please Tag these images so that the information can be permanently stored with the digital file.---Repository: San Diego Air and Space Museum
86908305 :Piction ID--Convair 990 - front portside view 11/01/1962---Please tag these photos so information can be recorded.---- Digitization of this image made possible by a grant from NEH: NEH and the San Diego Air and Space Museum
The FB-111A was intended as an interim aircraft between the B-52 and the Advanced Manned Bomber (which turned out to be the B-1B), and a replacement for the B-58 Hustler. It was something of a Frankenstein's monster, in that it used the airframe of the F-111A, the longer wings of the cancelled F-111B, and the newer Triple Plow II intakes, engines, and avionics suite of the F-111D. This suite was in turn even further upgraded with improved radar, navigation systems (including a primitive GPS), and bomb delivery system that allowed for fully automatic bomb runs even in poor weather. The landing gear was also strengthened to allow for a much higher maximum weight and warload; though the FB-111A could carry even more bombs than the tactical F-111 models, it carried AGM-69 SRAM standoff nuclear missiles in SAC service.
Once the B-1B Lancer was fully mission-capable, the FB-111s were no longer needed by SAC, and in 1989 they were redesignated F-111G and handed over to Tactical Air Command. There they served until sold to the Royal Australian Air Force in 1996 as attrition replacements for the RAAF's F-111K fleet; as such, they were among the last Aardvark variants retired, beginning in 2009.
Only eleven of the 76 FB-111s have been preserved, and this one, 68-0248, is a little mysterious. I have not been able to find which of the three FB-111 wings it served with, though it may have been with the 509th Bomb Wing (Medium) at Pease AFB, New Hampshire. Whichever unit it was with, 0248 was one of the FB-111s to receive nose art when the USAF briefly allowed it again in the late 1980s; it was named "Free For All" and has an attractive pinup in a bikini--on the right side of the aircraft, not seen in this picture.
68-0248 was retired in 1990 and preserved at the South Dakota Air and Space Museum at Ellsworth AFB. Initially, it retained its last camouflage scheme, the overall gunship gray worn by the F-111G fleet, but it was repainted around 2015 in SIOP camouflage used by the FB-111s in the 1970s and early 1980s. Unless I saw one when I was a kid, I believe this is the first time I've ever seen a FB-111.
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
While the F-16A had proven a success, its lack of long-range missile and true all-weather capability hampered it, especially in projected combat against the Warsaw Pact over Central Europe. General Dynamics began work on the upgraded F-16C/D version, with the first Block 25 F-16C flying in June 1984 and entering USAF service that September.
Externally, the only ways to tell apart the F-16C from the F-16A is the slightly enlarged base of the tail and a UHF radio antenna at the base of the tail. The intake is also slightly larger, though later marks of the F-16A also have this feature. Internally, however, the F-16C is a significantly different aircraft. The earlier APG-66 radar was replaced by the APG-68 multimode radar used by the F/A-18, which gave the F-16C the same capability to switch between ground-attack and dogfight mode and vastly improved all-weather capability. Cockpit layout was also changed in response to pilots’ requests, with a larger Heads-Up Display and movement of the radar display to eye level rather than between the pilot’s legs on the F-16A. The F-16C would also have the capability to carry the AIM-120 AMRAAM, though it would not be until 1992 that the missile entered service. Other small upgrades were made throughout the design, including the engine.
The Block 25 initial production was superseded by the Block 30 F-16C in 1987, which gave it better navigation systems, and the capability to carry the either the General Electric F110 or the Pratt and Whitney F100 turbofan. The Block 40/42 “Night Falcon” followed in 1988, equipped with LANTIRN night attack pods, followed by the Block 50/52, which was a dedicated Wild Weasel variant. In USAF service, the latter are semi-officially known as F-16CG and F-16CJ variants.
The F-16C had replaced the F-16A in nearly all overseas USAF units by the First Gulf War in 1991, and as a result, the aircraft was among the first deployed to the theater in August 1990. During the war, the F-16C was used mainly in ground attack and strike sorties, due to delays in the AIM-120, but it performed superbly in this role. USAF F-16s finally scored kills in the F-16C, beginning in 1992, when an Iraqi MiG-23 was shot down over the southern no-fly zone; the victory was also the first with the AMRAAM. Four Serbian G-4 Super Galebs were shot down over Bosnia in 1994. F-16Cs had replaced the F-16A entirely in regular and Reserve USAF service by 1997, and further service was seen over Kosovo, Iraq, Afghanistan, and Libya by 2012. Subsequent upgrades to USAF F-16Cs with GPS allow them to carry advanced precision weapons such as JSOW and JDAM.
Whatever the variant, the F-16 is today the most prolific combat aircraft in existence, with 28 nations operating the type (17 of which operate F-16Cs). Over 4450 have been built, with more in production; the F-16C is also license-produced by Turkey and South Korea. It also forms the basis for the Mitsubishi F-2 fighter for Japan, though the F-2 is significantly different, with a longer nose and larger wing. Though the USAF projects that the F-16C will be replaced by the F-35 beginning in 2020, it will likely remain in service for a very long time.
I don't know if the Thunderbirds intended this to form a heart in the sky, but it's a neat picture. This is actually a few seconds after the team completed a rolling diamond climb, with one of the solo aircraft coming up behind and then racing to meet the diamond at the bottom. It could be deliberate, as the Red Arrows do a heart formation (complete with arrow splitting the heart). This picture was taken at the Wings Over the Falls airshow in Great Falls, MT in July 2017.
F-111F. C.N. 54. 494th TFS at RAF Lakenheath. Flew in Operation Eldorado Canyon. Withdrawn from service to AMARC 19 October 1995 as AA FV0221. Scrapped at AMARC in June 2012. Photo Credit's: Unknown to me (Kodachrome Slide dated September 1992)
88483080 :Piction ID--Tomahawk missile near General Dynamics F-111---Please tag these photos so information can be recorded.---- Digitization of this image made possible by a grant from NEH: NEH and the San Diego Air and Space Museum
SAR-QC2 VTOL Aircraft
After going through many changes and cleaning it up. I'll be submitting this SAR-QC2 with USAF as per their solicitation request. Meets and dramatically exceeds requirements. Hydrogen Fuel Cell powered, and utilizing high pressure conforming tank technology I developed.
The underlying tech makes batteries for vtol absolutely obsolete, outright, forever. Also underlying tech results in ACTUAL fuel cell powered electric fixed wing aircraft and commercial aircraft. High pressure conforming tank technology, mixed with fuel cells, and composite aircraft construction. Results in radical advancements in capabilities. Not measured in minutes of endurance, but multiple hours of endurance
Screenshots with the smaller one, ie QC1 gives a size comparison. lnkd.in/e2_2AUV
vtol, air taxi, urban mobility, go fly prize, vertical flight, vertical flight society, usaf, afrl, afosr, darpa, dod, vtol, sbir, navair, diu, dia, arl, onr, mda, socom, afsoc, afwerx, boeing, lockheed, bae, raytheon, safran, utc, phantom works, skunk works, airbus, uber, safran, drone, us forestry, northrop grumman, general dynamics, nasa, hydrogen, fuel cell, vertical flight, vertical flight society, us army future command, space force, electric aircraft, e flight, evtol, additive manufacturing, honeywell, collins aerospace, cessna, piper, bombardier, gulfstream,
#usaf #afrl #afosr #darpa #dod #vtol #urbanmobility #sbir #navair #diu #dia #arl #onr #mda #socom #afsoc #afwerx #boeing #lockheed #bae #raytheon #safran #utc #phantomworks #skunkworks #airbus #uber #safran #drone #usforestry #northropgrumman #generaldynamics #nasa #hydrogen #fuelcell #goflyprize #verticalflight #verticalflightsociety #usarmyfuturecommand #spaceforce #electricaircraft #eflight #evtol #additivemanufacturing #honeywell #collinsaerospace #cessna #piper #bombardier #gulfstream
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Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
F-111F. C.N. 35. 493rd TFS at RAF Lakenheath. Withdrawn from service to AMARC 3 January 1996 as AA FV0242. Flew in Operation Eldorado Canyon. Photographed at RAF Boscome Down in June 1990. Scrapped in June 2012. Photo Credit's: Unknown to me (Kodachrome Slide)
PictionID:43057490 - Catalog:14_003937 - Title:Atlas 145D- Mariner Details: Mariner- 1; Atlas 145D On Pad; Test 2900 07/22/1962 - Filename:14_003937.TIF - - - - Image from the Convair/General Dynamics Astronautics Atlas Negative Collection---Please Tag these images so that the information can be permanently stored with the digital file.---Repository: San Diego Air and Space Museum
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
PictionID:42186274 - Title:Man in Spacesuit Emerging from Test Chamber-------7-11-62; 7 11 62 BW 4x5 , CROP - Catalog:14_002170 - Filename:14_002170.tif - - - - Image from the Convair/General Dynamics Astronautics Atlas Negative Collection---Please Tag these images so that the information can be permanently stored with the digital file.---Repository: San Diego Air and Space Museum
F-111F. C.N. 40. 493rd TFS at RAF Lakenheath. Seen here minus it's right, (or both), engine(s), Withdrawn from service to AMARC 9 January 1996 as AA FV0253. Scrapped at AMARC in June 2012. Photo Credit's: Unknown to me (Kodachrome Slide dated May 1980)
PictionID:43057067 - Catalog:14_003902 - Title:Escape Tower Details: Erection and Mating of Escape Tower on Capsule VIII 08/14/1961 - Filename:14_003902.TIF - - - - Image from the Convair/General Dynamics Astronautics Atlas Negative Collection---Please Tag these images so that the information can be permanently stored with the digital file.---Repository: San Diego Air and Space Museum
Catalog #: 10_0009650
Date: 1960-1969
Title: Convair/General Dynamics Atlas
Corporation Name: Convair/General Dynamics
Additional Information: Sycamore Canyon Static Test
Tags: Convair/General Dynamics Atlas, Sycamore Canyon Static Test, 1960-1969, Convair/General Dynamics
Repository: San Diego Air and Space Museum Archive
88088828 :Piction ID--Cruise missile comparisons---Please tag these photos so information can be recorded.---- Digitization of this image made possible by a grant from NEH: NEH and the San Diego Air and Space Museum
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive
USN F-111B Aardvark BuNo 151972 and USAF F-111A Aardvark reportedly s/n 63-9772, WSL, China Lake, Feb 1995. Copyright photo by Joe Cupido.
Willard Martin (b. 1917) held various jobs before he was hired by Convair San Diego as a metal worker. For the next 30 years, Martin worked at Convair, eventually serving much of his career as the Operations General Supervisor, a task that involved supervising experiment department operations, engineering test lap support, model shop operations, mockup and wind tunnel support. In addition, he managed all instrumentation fabrication, installation and field support operations for the Cruise Missile Program and others. In 1976, he was elected by members of the National Management Association, General Dynamics Convair Chapter, as Director of Public Relations from 1976 to 1977.
Repository: San Diego Air and Space Museum Archive