When
Saturday, March 4, 2023 from 12:00 PM to 1:30 PM PST
Add to Calendar
Tentative Agenda: (All Time PST (GMT -0800)) (US and Canada)
12:00 pm: Welcome and Introduction
12:05 pm: Presentation
01:05 pm: Q&A
01:35 pm: Adjourn.
Where
*****This is a hybrid meting, with in-person and online attendance. The speaker will speak online.
*In-person attendance:
Lawndale Library (Meeting Room)
14615 Burin Ave., Lawndale, CA 90260
(South of 105 Hwy and East of 405 Hwy/Pacific Coast Hwy (1))
(Near SpaceX Hawthorne, and close to Northrop Grumman Space Park)
(also online for a hybrid event)
(This event is not sponsored by the Lawndale Library)
*Online attendance:
Zoom connection information will be provided in the confirmation email after registration / RSVP.
Contact
American Institute of Aeronautics & Astronautics, Los Angeles - Las Vegas Section
949-426-8175 events.aiaalalv@gmail.com
(This meeting is cancelled due to clearance issues.) (Apologies.)
You are encouraged to join earlier for the first exciting talk on March 4 @10:30 AM PST, RSVP and Information: https://conta.cc/3Y2IBbZ
Thank you so much again. Wish you could join us at 10:30 AM PST for another talk, and / or in upcoming AIAA LA-LV meetings.
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AIAA LA-LV 3/4 Section Town Hall Meeting (Hybrid)
Saturday, March 4, 2023, 12:00 PM - 1:30 PM PST (GMT -0800)(US and Canada)
A Brief History of An Aerospace Structural Engineer
(An AIAA LA-LV Section Hybrid Meeting)
by
Frederick Palmieri
Engineering Fellow at Raytheon SAS
(The speaker will present online remotely.)
Lawndale Library (Meeting Room)
14615 Burin Ave., Lawndale, CA 90260
(South of 105 Hwy and East of 405 Hwy/Pacific Coast Hwy (1))
(Near SpaceX Hawthorne, and close to Northrop Grumman Space Park)
(also online for a hybrid event)
(This event is not sponsored by the Lawndale Library)
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(If you are sick or don't feel well, please stay home and attend online on Zoom.)
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(Please don't type anything in the Promo Code area. The discounts/promotions have been reflected directly in the ticket price list for selection. No Promo Code is needed.)
(Any special ticket request or for group rate, please contact events.aiaalalv@gmail.com)
(Your generous donations will be welcome and appreciated, but not required.)
(https://www.paypal.com/donate/?hosted_button_id=QTN5D6G64RZGA)
COVID-19 Pre-cautions:
The Indoor Mask Mandate has been lifted. It's recommended to wear a mask indoors, but it's not required. (If you are sick or don't feel well, please still stay home and attend online on Zoom.) If you booked with in-person tickets, but realized you can't make it in-person, please inform us ASAP. Each in-person ticket will include the online access as well.
(Dress Code: Business Casual)
(In-person attendees: Indoor masks are recommended, but not required. But please respect each other, especially if some feel better with social distancing. If you're sick, please stay home and attend online.) -----------------------------------------------------------------------------------
Frederick Palmieri
Frederick Palmieri possesses over 60 years of hands-on experience with structural, structural dynamic, fatigue and fracture mechanics analyses of aircraft, helicopter, and missile structural components. Specifically, commencing in 1954, he performed stress, dynamic and fatigue analyses of the Radioplane XQ-5 drone, similar analyses for the Piasecki H-12 and H-16 helicopters, and analyses of aircraft pods, engine pylons and over/under wing structure for the Boeing 707-120, Convair 880 and Lockheed Electra for Rohr Aircraft Company.
He also performed stress analyses for the Mc-Donnell F-101B center fuselage and the wing structure of the AVRO CF-105b. At Lockheed Missiles and Space Company he was Section Head of Basic Loads and Criteria, helping to develop the six degree of freedom software for launch and guidance of the Polaris Intercontinental Ballistic Missile
He was the Department Head for the structural, thermal, and dynamic analyses for the AVCO heatshield and underlying structure of the Apollo Command Module. Beginning in 1984 while acting as a consultant to Hughes Aircraft Company, he was the lead structural engineer for the ASTOR and E-10A radar pods and contributed to stress, dynamic and fatigue analyses for the MP-RTIP radar pod. Since January of 2009 he has performed structural, dynamic and fracture mechanics analyses for several different aircraft systems and currently, the B-52H radar.
Frederick obtained a B.S. degree in Mathematics and an M.S. degree in Engineering Mechanics from Stanford University and continued in pursuit of a Ph.D. under the guidance of Professor Donovan Young. However, on Dr. Young’s retirement he came to a disagreement with his new advisor, Tom Kane, and dropped out of the program. Later he continued his studies to complete the requirements for a Ph.D. from an on-line university and published a thesis (“A Preliminary Study of the Structural Dynamic Behavior of the NASA Manned Spacecraft Center (MSC) Centrifuge,” IBSN: 1-58112-206-3). He holds two published patents, the latest assigned to Raytheon.
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