Thor
by
Jean-Jacques Serra
Origins
Thor Able
Thor Ablestar
Thor Agena
Thor Delta
Thor with solid top stage (Altair, Burner)
Origin: first generation of American Intermediate Range Ballistic
Missiles
Until 1953 the USAF had stressed on aerodynamic missiles (while the Army was
developping the Jupiter) because they believed long distance ballistic missiles
would not appear before ten years. The construction of Thor wasn't awarded to
Douglas Aircraft before December 1955. The program was given a very high
priority and the first missile was delivered to the USAF in October 1956.
The MB-1 propulsion system was made of a Rocketdyne LR79 (liquid oxygen and
kerosene) engine with 670 kN derived from Jupiter and
Atlas'
booster. An LR101 vernier rocket on each side of the missile' base controled
the roll and the final ajustement of the speed after the main engine shutdown.
The missile used
Atlas'
Reentry Vehicle, measured 2.44 m in diameter and 19.8 m in height, and weighed
over 46 tons.
The first four tests carried out from 25 January 1957 on were failures. The
first successful launch occured on 20 September and was commissioned in
1959.
Thor's propulsion system quickly evolved to an MB-3 version used by IRBMs and
space launchers, especially by USAF's Thor SLV-2 and NASA's
Thor Delta
launchers. In the seventies the MB-3 motor was used by the Japanese N-1, N-2
and H-1 launch vehicles. An improvement program conducted between 1957 and 1959
named X-1 leaded to an H-1 version designed for Saturn-1. Later on H-1 was
modified for the propulsion of
Thor Deltas
(39xx series) and became RS-27. The latest version RS-27A intended to Delta-2
launchers is optimized for greater performance at high altitude.
Designation
|
Year
of first launch
|
Main
engine Thrust (kN)
|
Main
engine SI (sec.)
|
Application
|
MB-1
|
1957
|
600
|
250
|
IRBM
|
MB-3
|
1958
|
670,
735, 755 (1)
|
252
|
IRBM,
launchers
|
RS-27
|
1973
|
920-1030
(2)
|
263-295
(2)
|
Delta
|
RS-27A
|
1991
|
890-1055
(2)
|
255-305
(2)
|
Delta-2
|
Notes: (1) Blk 1, 2 and 3; (2) values given at sea level in vacuum
In 1963 Thor's thrust became insufficient to carry out its missions. The
solution (innovative at that time) found was to enhance it with 3 solid fuel
strap on Thiokol
Castor
boosters. This resulted in TAT: Thrust Augmented Thor. Those boosters were used
grouped by 3 then 6 and up to 9. After 1975 when the only Thor first stage used
was the Delta the
Castor-2
boosters were replaced by the 1 m-diameter
Castor-4.
The burn duration of Thor (160 seconds) was also enhanced by lenghtening its
tanks. This gave birth to the LTT (Long Tank Thor) for which the burning time
reached about 220 seconds, used from 1966 wih
Agena
stages and from 1968 with Delta stages. The first stage was streched again in
early 70' giving ELTT (Extended Long Tank Thor); the burning time wasn't much
modified but the thrust was increased. The Delta-2 version, used since 1989,
was lengthened in order to obtain a 265 seconds burning time.