SP-4012 NASA HISTORICAL DATA BOOK: VOLUME III
PROGRAMS AND PROJECTS 1969-1978
 
 

Table 1-34. Titan IIIC Characteristics.

 

.

Stage O Solid Rocket Motors (2)

1st Stage Titan

2d Stage Titan

3d Stage Transtage

Total

.

Height (m):

25.9

22.2

7.1

9.4

38.7

Diameter (m):

3.05

3.05

3.05

3.05

-

Launch weight (kg):

226 800 each

123 830

33 112

16 500

400 242

Propulsion system

Powerplant:

United Technology 1205

Aerojet YLR87- AJ-II

-

-

-

Thrust

10.45 mill (combined)

2.16 mill

-

-

-

Burn time (sec.):

110

150

108

420

-

Propellant:

powdered aluminum/ ammonium perchlorate

N2H4-UDMH/N204

N2H4 -UDMH/ N204

N2H4 -UDMH/ N204

-

Payload capacity:

10 443 kg to earth orbit

1202 kg to Mars

Origin:

Air Force Titan missile

Contractors:

Chemical Systems Div., United Technologies

Martin Marietta Corp.

-

-

-

Program manager:

Theodrick B. Norris, NASA Hq.

Project manager:

Andrew J. Stofan, Lewis Research Center

How utilized:

ATS

Remarks:

NASA and the Air Force signed a memorandum of understanding allowing NASA to use this Air Force vehicle for the ATS project on Feb. 6-7, 1970.

The second ATS mission (ATS G) was cancelled in Jan. 1973. ATS 6 was launched successfully on May 30, 1973.


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