Atlas
by
Jean-Jacques Serra
Launchers operated by Lockheed Martin Launch Services, formerly General
Dynamics. Since mid-1995 the launchers are marketed by
ILS
http://www.lmco.com/ILS/
Origins of Atlas
Atlas without top stage
Atlas with an Agena stage
Atlas with solid top stage
Atlas with a Centaur stage
Origin: Inter Continental Ballistic Missile (ICBM) of first
generation
In January 1955 the General Dynamics' Convair division was selected to build
the Atlas system. In 1946 this firm was awarded a contract to design a 8000 km
range ICBM: the MX-774. Three of those were launched in 1948 before the project
was cancelled. Notheless those studies had lead to 3 major innovations: the
engine with gimbaled nozzle, the monocoque structure and the releasable
payload.
In the mid-50ies the problems related to high altitude ignition of liquid ergol
engines were not solved. The only known solution was to ignite them all at
takeoff: the Russians picked a bundle structure for their
Semiorka
while the Americans opted for a one-and-a-half stage vehicle. A main Rocketdyne
LR105 sustainer of 670 kN was supported by 2 LR89 boosters. The propulsion bay
containing 3 motors was named MA-1. Those engines consumed ergols (liquid
oxygen and kerosene) provided by the same tanks. On each side a vernier LR101
rocket of 4.45 kN provided fine tuning of the thrust. The missile itself was
3.05 m diameter and 22.9 m in height (with an Mk2 Reentry Vehicle) and weighed
over 110 tons.
On 11 Jun 1957 for its first test, the missile was only propulsed by its
lateral motors... but it failed. The first success occured at the third try, on
17 Dec 1957. On 2 Aug 1958 the first 3-motor Atlas (named version B) ranged
over 4000 km and the nominal range was achieved on 28 Nov 1958 (version C).
Less than a month later on 18 Dec 1958 Atlas was used for a space mission:
Score.
The propulsion system kept on evolving, first as a missile then as a space
launcher. The first improved MA-2 was used for the Atlas-D ICBM. Then the MA-3
was introduced as a simplified version for the Atlas-E and -F ICBMs and derived
launchers. The MA-5 was a civilian version of the MA-2; it was used by Atlas
SLV-3 until the MA-5A version became available for Atlas-2.
Designation
|
Year
of first launch
|
Main
engine Thrust (kN)
|
Main
engine SI (sec.)
|
Additional
engines Thrust (kN)
|
Additional
engines SI (sec.)
|
Application
|
MA-1
|
1957
|
240
|
210
|
1335
|
245
|
Atlas
A, B, C
|
MA-2
|
1958
|
255
|
213
|
1375
|
248
|
Atlas
D
|
MA-3
|
1960
|
255
|
214
|
1470
|
250
|
Atlas
E, F, launchers
|
MA-5
|
1961
|
270
|
220
|
1680
|
259
|
launchers
|
MA-5A
|
1991
|
270
|
220
|
1885
|
264
|
launchers
|
Atlas was equipped with the top stages of
Thor Able
-derived from those of Vanguard- in 1959. This launcher named Atlas Able was to
launch the Pioneer probes to the Moon. But after 3 failures between November
1959 and December 1960 it was abandonned.
Between 1956 and 1989, 189 MA-1/MA-2, 238 MA-3 and 213 MA-5 propulsion
systems were manufactured that is 640 Atlas. The great majority of those Altas
were used as ICBM. Thus the 150th Atlas was fired on 7 Nov 1962 and within
those 150 rockets only 31 did launch satellites.