Brovetto, Ronald, MSgt

Security Forces

Service Photo

Service Details

Current Service Status
USAF Retired

Current/Last Rank
Master Sergeant

Current/Last Primary AFSC/MOS
3P0X2-Law Enforcement

Current/Last AFSC Group
Security Forces

Primary Unit
2007-2021, 3P0X1, 163rd Attack Wing

Previously Held AFSC/MOS
3P0X1-Security Forces

Service Years
1986 - 2021

Official/Unofficial US Air Force Certificates

Cold War Certificate

Official Badges

Unofficial Badges

Military Associations and Other Affiliations


	1986, American Cold War Veterans - Assoc. Page
	1990, National Rifle Association (NRA)
	2010, Air Force Security Forces Association, Inland Empire Chapter (Associate Member) (Riverside, California)
	2010, Veterans of Foreign Wars of the United States (VFW), Post 233, Desert Edge Post (Member) (Beaumont, California) - Chap. Page
	2019, American Legion, Post 1379 (Member) (Stamford, New York) - Chap. Page

Photo Album (More...)

Iraq 2008

1986-1990, LGM-30G Minuteman III Missile

From Year 1986	To Year 1990

Personal Memories

Counter Drug missions, CA Dept of Justice CAMP program.

Image	LGM-30G Minuteman III Missile Details
	Aircraft/Missile Information The LGM-30G Minuteman III program started in 1966, and included several improvements that distinguish it from the LGM-30F Minuteman-II. Most modifications related to the final stage and re-entry system. The re-entry system developed for the LGM-30G was capable of deploying penetration aids (chaff) and up to three re-entry vehicles with and overall increase in payload delivery as well. The introduction of multiple re-entry vehicles on a single ICBM was a significant advance in the development of strategic nuclear missiles that substantially increased their threat. TECHNICAL SPECIFICATIONS General Information Developed by USA Deployed by USA Development Year 1966 Deployment Year 1970 Retirement Year 2020 Platform In hardened silos Number deployed 550(F.E.Warren AFB(150), Malmstrom AFB(150), Minot AFB(50), Grand Forks AFB(50))(as of 1997) Contractor Boeing Co., Military A/C & Missile System Div. Dimensions and Performance Length 18.2m Body Diameter 1.68m(1st stage) , 1.32 m(2nd stage), 1.32 m(3rd stage) Launch Weight 35,400kg Range 13,000km (Mk-12 RV), 11,300 km (Mk-12a RV) Speed 6.7 km/sec Altitude 1,130 km Accuracy 280m (Mk-12 RV), 120m (Mk-12a RV) CEP Components Propulsion 3-stage solid propellant Engine Thiokol TU-122(M-55) solid fuel motor(1st-Stage), Aerojet General SR19-AJ-1 solid fuel motor (2nd-Stage), Aerojet and Thiokol SR73-AJ-1 solid fuel motor (3rd-Stage), Rocketdyne RS-14 restartable liquid fuel motor (PostBoost Stage) Payload 3 Mk 12A RVs + penetration aids (includes chaff and decoys) Warhead 3 W-78s (335-350kT) ; Under START-II (if it is implemented) the current three warhead MIRV loading will be changed to a single 300 Kt W-78/Mk-21a each (taken from the to-be-retired Peachekeeper force) Guidance Inertial (INS-20 : all-inertial, gimbaled, improved NS-20 guidance system system manufactured by Autonetics Division, Rockwell International.)