Chandler, John Seymoure, Brig Gen

 Service Photo   Service Details
10 kb
View Time Line
Last Rank
Brigadier General
Last Primary AFSC/MOS
2746-Research and Development Officer, Special
Last AFSC Group
Command and Control
Primary Unit
1966-1968, Aeronautical Systems Division
Service Years
1943 - 1972
Officer Collar Insignia
Brigadier General

 Last Photo   Personal Details 

Home State
Year of Birth
This Military Service Page was created/owned by CCM Robert D. Chandler (Dan) to remember Chandler, John Seymoure, Brig Gen USAF(Ret).

If you knew or served with this Airman and have additional information or photos to support this Page, please leave a message for the Page Administrator(s) HERE.
Contact Info
Home Town
Roundup, MT
Last Address
Not Specified

Date of Passing
Sep 30, 1986
Location of Interment
Arlington National Cemetery - Arlington, Virginia
Wall/Plot Coordinates
Columbarium Court 7, Section NN, Column 24, Niche

 Official Badges 

Strategic Command Defense Information Systems Agency Missileman (Basic) Headquarters Air Force

Commander Air Force Retired

 Unofficial Badges 

Cold War Medal

 Additional Information
Last Known Activity
Not Specified
Other Comments:
Not Specified
 Photo Album   (More...

 1956-1963, SM-68/HGM-25 Titan I Missile
From Year
To Year
Personal Memories
Not Specified
 SM-68/HGM-25 Titan I Missile Details

Aircraft/Missile Information
The Martin B-68 Titan took over the designation after the Martin XB-68 bomber project was canceled.
The B-68 Titan I was redesignated SM-68 and later changed to HGM-25A.
The Titan II was reassigned the LGM-25C designation.
First launch of a SM-68 Titan I was Feb. 6, 1959
The Titan I is easily distinguished from the Titan II by noting the Titan I has a smaller diameter upper stage (the Titan II is constant diameter first and second stages). The Titan III and IV series rockets have two solid propellant strap-on first stage boosters.

Length: 103 ft. (ICBM configuration); first stage length 70 ft.
Diameter: 10 ft. (first and second stages - ICBM configuration)
Weight: 270,000 lbs. at launch
Armament: General Electric Mk. 6 Nuclear warhead
Engines: First stage powered by Aerojet LR87-AJ-5 two chamber liquid propellant rocket of 430,000 lbs. thrust fueled by Aerozine-50 (fuel) that ignites on contact with nitrogen tetroxide (oxidizer); second stage of ICBM configuration powered by Aerojet-General LR91-AJ-5 rocket engine of 100,000 lbs. thrust
Crew: None

PERFORMANCE (ICBM configuration):
Maximum speed: 15,000 mph / 13,904 knots
Maximum range: Approx. 10,000 statute miles / 8,700 nautical miles
Maximum altitude: 700 statute miles / 610 nautical miles

Add your memories to this entry

Last Updated: Dec 15, 2014
My Photos From This Aircraft/Missile
No Available Photos

  34 Also There at This Aircraft:
  • Anderson, James, A1C, (1958-1966)
  • Arrowsmith, Arthur, A2C, (1958-1962)
  • Byer, Dale, MSgt, (1956-1976)
  • Cissell, Robert, A1C, (1959-1963)
  • Davis, Hugh, A1C, (1963-1967)
  • Donnelly, Terrence, A1C, (1960-1964)
  • Flanders, David, TSgt, (1962-1970)
  • Freeman, Harry, A1C, (1955-1964)
  • Garrison, Jeanie
  • Holmes, George, MSgt, (1951-1974)
  • Hughes, James, A1C, (1960-1964)
  • Karsner, David, SMSgt, (1950-1974)
  • McNamara, James, CMSgt, (1961-1989)
  • Peck, Robert, MSgt, (1960-1981)
  • Roof, Robert, A1C, (1961-1965)
  • Skalski, Steve, Sgt, (1962-1965)
  • Sparks, James, A1C, (1958-1964)
  • Turner, David, A3C , (1961-1965)
  • Uhrmacher, Sherwood, MSgt, (1952-1973)
Copyright Inc 2003-2011