This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Titan 3A

Titan 3A
Titan 3A - Titan 3A - COSPAR 1965-008

21,243 bytes. 138 x 525 pixels.



Family: Titan. Country: USA. Status: Hardware. Department of Defence Designation: SLV-5A.

Titan with Transtage third stage. Core for Titan 3C.


Specifications

Launches: 4. Failures: 1. Success Rate: 75.00% pct. First Launch Date: 01 September 1964. Last Launch Date: 06 May 1965. LEO Payload: 3,100 kg. to: 185 km Orbit. Liftoff Thrust: 197,510 kgf. Total Mass: 161,730 kg. Core Diameter: 3.1 m. Total Length: 42.0 m. Flyaway Unit Cost $: 30.74 million. in 1985 unit dollars.


Titan 3A Chronology


1964 Sep 1 - LV Configuration: Titan 3A s/n 3A-2. Launch Site: Cape Canaveral . Launch Complex: LC20. FAILURE: Failure.
1964 Dec 10 - LV Configuration: Titan 3A s/n 3A-1. Launch Site: Cape Canaveral . Launch Complex: LC20.
1965 Feb 11 - - 15:19 GMT. LV Configuration: Titan 3A s/n 3A-3. Launch Site: Cape Canaveral . Launch Complex: LC20.
1965 May 6 - - 15:00 GMT. LV Configuration: Titan 3A s/n 3A-6. Launch Site: Cape Canaveral . Launch Complex: LC20.

Bibliography:



Titan 3ATitan 3A

Credit: © Mark Wade. 2,146 bytes. 59 x 565 pixels.



Titan LVs SmallTitan LVs Small

Credit: © Mark Wade. 5,757 bytes. 373 x 293 pixels.



Titan 3A LargeTitan 3A Large

Credit: © Mark Wade. 669 bytes. 28 x 225 pixels.



Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .