.
.
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.