Hassan Saberi Irvine, Ca ad2vz6@r.postjobfree.com 714-***-****

PROFESSIONAL SUMMARY

Sr. Principal System Engineer Scientist (GMD) and Electromechanical design Manager (Space shuttle) with extensive experience on NASA, Air Force, Navy, and as a contractor commercial airplane system .

EDUCATION:

M.S. Mechanical/Structural Engineering, California State University, Long Beach, CA

B.S. Civil Engineering, University of Nebraska, Lincoln

California Community Colleges – Engineering Instructor credential

PROJECTS:

777X Pilot control System (PCS) / Primary Flight Function (PFF); Rescue Hoist & Winch; Auto injector/pill dispenser medical devices; Hydraulics Motion Control Valve, Flush Control; Space Launch Systems; GPS III, Ground Based Interceptor (GBI) & Aegis ballistics’ Missile Defense (10 yrs.) and Space Shuttle (20 yrs.).

Performed aerospace systems engineering architecture, requirements decomposition, allocation, flowdown and traceability using DOORS

Interface definitions, risk, TPMs, trade studies and end-to-end “V” process throughout design, MFG, integration, test, verification, and sustainment.

Managed requirements verification/validation/certification) for more than 5000 requirements using DOORS

In depth knowledge of FAA DO-160, Mil-STDs-1540/810/461, NASA-STDs 5010/5019, ISO-11608, ISO13485, ASTM D4169 etc.

Prepared Qualification Test (QT) plan,, Acceptance Test (AT) procedures and Reports, Compliance matrices, and Verification reports:

Performed ENV tests e.g., shock, vibe, pressure, humidity, temperature, life, HALT, etc.

Performed EMI tests e.g., Conducted & Radiated RF Susceptibility, RF Conducted & Radiated Emissions, ESD, etc.

Prepared Failure Analyses Reports using 8D, Fault Tree, etc.

Analyzed: Design fatigue, damage tolerance, endurance limits, fracture control, fungus, NDE, etc.

Prepared aerospace electromechanical BOMs, conceptual designs, preliminary designs:100s of Details, Assemblies and Installations drawings using CAD tool and GD&T standards.

Member of MRB and provided MR dispositions and problem resolution with Corrective Actions

Prepared presentations and presented to:

Internal technical team e.g., MRB, FRB, ERB, CCB, MRR, TRR

Customers e.g., TIM, SDR, SRR, PDR, CDR, FRR, etc. with signature authority.

Test Data analyzer and experienced user of Power Point, MS Word, Excel, MS project tools and design history data base CDOCS, ENOVIA, PDM, EBOM, etc.

Security Clearance: DOD Secret from 1986 through 2014 – INACTIVE

PROFESSIONAL EXPERIENCE:

Boeing 777X Primary Flight Control Function Requirement V&V 09/2022 – Jan 2024

Guidance Navigation & Control - Principle System Engineer

Performed PFF decomposition assessment and allocation traceability using DOORS.

Prepared and presented change proposal package for Requirements Review Board (RRB) approval.

Investigates actions necessary for requirements definition, decomposition and flow-down.

Develops certification criteria and methods with regulatory agencies.

Performs a wide variety of complex trades studies to meet program requirements.

Collins Aerospace – Rescue Hoist and Winch System Brea, Ca 09/2021- 06/2022

Sr Test and Sustainment Engineer

Investigated Hoist & Winch field failure and provided root cause with corrective actions reports

Supply chain engineer for wire harnesses, drum housing casting, etc.

Test lead for rescue hoist drum housing casting tensile, fatigue and destructive tests.

Amgen Pharmaceutical - Auto injector medical device 12/2020-7/2021

Principal System Engineer

Provided system requirement development of system architecture and integration of subsystems ensuring a robust system architecture across dependencies and the interfaces of subsystem.

Device constituent e.g., compatibility, sterility, sharp protection; packaging; labeling, functional performance; reliability (storage; safety), biocompatibility, ICD, regulations (ISOs ASTM, CFR, or FDA)

Supported system requirements management using DOORS, design, test and MFG life cycles from characterization, clinical verification, MFG, commercial validation for user need market.

Supported environmental testing IAW MIL-STD-810F, ISO-11608 & ASTM D4169 e.g., transportation vibration, shock, drop tests, hot/cold temperature tests, shelf life and accelerated aging tests.

Supported functional tests e.g., Cap removal force, activation force, hold force, Injection Time (IT), needle shield clearance, needle extension measurements and verification of drug delivery system and subsystems devices.

Supported Final Assy Break Loose Extrusion (BLE) test force vs velocity and component device output power testing force vs displacement to determine IT variabilities, Alert Limit factor and BLE damping. coefficient.

Prepared design transfer Plans and reports for MFG

Eaton Aerospace – Hydraulics Fuel & Pneumatics motion control system - Irvine, CA 12/2019 – 4/2020

Senior Project Engineer – Contract was on hold and ended because of Covid-19 pandemic

Performed Qualification Test (QT), l Acceptance Test (AT) using DO-160, MIL-STD-810 and prepared QT & AT reports for Northrop 1” valve motion control fuel system:

Operational, proof and burst pressures, temperature variation, fuel temperature, shock, vibration, humidity, external pressure, Icing, etc.

Prepared compliance matrices (8) for Lockheed New Ejector Pumps Products

Zodiac Aerospace – Flush Control System Test Engineer- Carson, CA 09/2018 –3/2019

Sr project Engineer

Performed A320 & A380 proof, burst pressures, temperature variation, 7 cycles freeze, life cycle tests using DO-160 and MIL-std-810 and prepared Qual Test reports

Performed HALT and determined Upper, Lower Operational, and destructive Limits for hot, cold, vibration, voltage and combined vibe, temperature, and voltage. Prepared HATL test report

Rockwell Collins – 777X/787 Pilot Control System Irvine, Ca 08/2016 –07/2018

Senior System Engineer

Authored Qual by similarity (QBS) reports for PCS 777X using 787 Qual test data & analyses:

Prepared and or reviewed Qual Test (QT) Plan, Procedure using DO-160 and Mil-STD 810 for environmental QTs covering Vibration, Shock, Acceleration, Loads, Endurance, Temperature, Overpressure, Humidity, Noise, Decompression, E3 (Conducted/Radiated RF Susceptibility, RF Conducted/Radiated Emissions), etc.

Prepared verification compliance matrices i.e., artifacts and report for 777X 4200 requirements.

Managed requirements in DOORS and Validated PCS Specification Control Document (SCD) requirement flow down and its 6 components requirement traceability: Thrust Control, Speedbrake Stabilizer and Pedestal Control Modules, Alternate Pitch Trim/Parking Brake, Flap and Alt Flap Control Modules

Prepared material science fungus analysis report using D0-160, MIL-HDBK-454

Parker Aerospace – Space Launch System (SLS), 08/2015 –8/2016

Senior Project Engineer

Authored Hydraulic Quick Disconnect (HQD) Fracture Control report providing NHLBB, Low Risk, fail-Safe, endurance limit analyses using SMC-S-016, NASA-STD-5019 and NASA-HDBK-5010, MIL-STD-810

Prepared HQD and Hydraulic Flex Hoses (HFH) Qual Test (QT) plans, procedures

Prepared HQD & HFH Material ID Usage List (MIULs) reports using NASA’s MAPTIS.

Performed damage tolerance, NDE, Qual/Acceptance tests, assessments, validation, and verification for operational & non-operation environments:

Nominal Operating Pressure: Max Operating/expexted, Proof, Burst, Impluse pressures, flow rate, pressure drop, and structural life performance Reqts.

Ops and Non-Ops environments::Shock, Vibe, temperature variation, Thermal vacuum, pressure rate/flow/drops, humidity, acceleration, salt, fog, Structural loads, mass properties, limit loads, etc.

Flextronics- Pharmaceutical Irving, TX 01/2014 –05/ 2014

Sr System Engineer - Short-term contract

Prepared fishbone failure report defined and allocated requirements for customer dispensing system. Prepared Product Requirement Specification of electromechanical dispensing system

AEROSPACE CORP, Navigation Division-GPS, El Segundo, CA 8/2010 - 11/2013

Senior Project Engineer - Requirements managements: decomposition, and flow down

Reviewed and approved 300 Requirement Verification Plans with artifacts for GPS III segments (space, user, and control), internal & external interface

Monitored Tech Performance Measures, risks, system capabilities and thread

Performed risk reduction, studies, simulation and developed Civil Code test vector.

Reviewed and recommended disposition of changes for GPS III & GPS II system segments Specs and ICDs for more than 3000 requirements & 100 Deviations & Waivers using Military standards 810, 1540, 1791, 1547, 461/464, etc. and coordinated reviews for ERB & CCB.

Reviewed and approved GPS III requirements, ICD, other governments, and prime contractor Specs. & ICDs e.g., Boeing, LM, L3, Rockwell, etc.:

Monitored Tech Performance Measures, risks, gaps, system capabilities and threads.

Performed risk reduction simulation test and developed Civil Code test vector report.

BOEING- Sr. Principal System Engineer Scientist and Design Manager 2/1981- 9/2010

Ground-based Missile Defense (GMD) & Aegis Ballistic Missile Defense (ABMD) lead 2001– 2010

Authored GMD Interceptor (Boost Vehicle & its Payload) Data Book

Used DOORS to Prepare Prime Items & Critical Items Developments Specifications (PIDS & CIDS) and their ICDs & SCDs, ensured requirements were linked, traced, compatible, complete, consistent, clear, and accurate for more than 1700 requirements

Prepared verification/validation reports for more than 1700 of SM-3 Kinetics Weapon (KW) & GMD requirements.

Supported booster and KW payload Integration & Test (I&T) at contractors (Orbital Science Corp, Raytheon), VAFB and Huntsville

Troubleshooting acceleration, pressure, acoustic, strain and thermal sensors issues. Dispositioned more than 400 MRs, Deviations & Waivers.

GMD: Reviewed and approved Interceptor PIDS, and Interface Specifications and ICDs for more than 1000 requirements.

GMD: Developed Max. Predicted Environments (MPE) and verified Electromechanical System design, stress and dynamics analyses for Operational & Non-Operational environments e.g., humidity, pressure, temperature, stress, shock, vibration, acoustics, E3 and mass property for more than 500 requirements.

ABMD: Used DOORS to Develop and allocate requirements for SM-3 KW PIDS and its components (ejector, transmitter, battery, PCU, Antenna, etc.) for more than 1200 requirements

ABMD: Performed Qualification testing e.g., vibration, shock, acoustics pressure, humidity, temperature, E3 (Conducted/Radiated RF Susceptibility, RF Conducted/Radiated Emissions, etc.) and verified 1200 requirements...

Space Shuttle Subsystem Manager - Mechanical Structure IPT 02/1981-11/2001

Led 6 engineers responsible for electromechanical design and development of space shuttle payload structures, shuttle airframe and its ICDs for more than 1000 drawings

Integrated and tested over 100 shuttle missions USING NASA, Military & FAA STDs

Member of MRB with signature authority for more than 1500 MRs, Waiver & Deviations and real time lunch support and chaired problem resolution team

NASA certified Subsystem manager and certified 50 Orbiter Rollout and Flight Readiness reviews

Prepared conceptual, preliminary layouts, over 100s of Details, Assembly, Installation drawings using CATIA and GD&T standard

Provided MR dispositions and problem resolution.

Quality product IAW D & C guidelines e.g., corrosion protection, plating, fasteners & material selection, tolerance stack-up calculations, etc.

CERTIFICATIONS / HONORS:

NASA certified System Integration Subsystem Manager.

Air force DoD certified Responsible Engineer

Many NASA (Space Shuttle), Air Force GMD, Navy ABMD and Boeing Awards

REFERENCES: will be furnished upon request.

Contact this candidate