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SPACECRAFT DESCRIPTION
L The Spacecraft for the AS-50_ mission is composed of:
Launch Escape System (LES)
Command Module (CM)
;. Service Module (SM)
Lunar Module (_I)
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Spacecraft Lunar Module Adapter (SLA)
Launch Escape S_ste m
The Launch Escape System, which is Jettisoned approximately 35 seconds after
S-II Ignition, is made up of a Launch Escape Tower (LET), and a three-motor pro-
pulsion system (Tower Jettison, Launch Escape and Pitch Control Motors).
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; "Command Module
The Command Module is a Block II Configuration. The module's inner struc-
ture, or pressure vessel, is separated fzom the outer structure by a layer of
" insulation. A heat shield structure is made up in three segments consisting of
a forward heat shield, a _rew compartment hea_ shleld_ and an aft shield. The
(24 is slightly over ii feet in length and is about 12 feet in diameter. A"
• propulsiot_ system consists of Reaction Control Engines which may operate pulsed
or continuous.
Service Module
' The Service Module maybe described as a cylindrical, aluminum shell which
• is mad& up of honeycomb-sandwich panels and a forward and aft bulkhead. Oke
gimballed propulsion engine (capable of up to 30 restarts) and a reaction control
system (4 clusters, 4 chambers each) make up the Sl! Propulsion System. The Com-
mand and Service Module are Joined by three tension ties each of which is
equipped with explosive charges for SM/CMseparation.
Lunar Module
The Lunar Module consists primarily of an Ascent and Descent Stage. The
Ascent Stage, which contains the crew compartmettt_ is equipped with a Reaction
Control System which provides thrust capability, an ingress and egress hatch to
the _rew's instrumentation and controls. The Descent Stage_ consists primarily
. of a descen_ engine a,d four retractable landing gear assemblies. Over all
, weight of the Lunar _odule is approximately 30,000 pounds. -"
Spacecraft Lunar Module Adapter
The spacecraft Lunar Module Adapter (SLA) Joins the S_rvlce Module (SM) to
the S-IVB/IU. The SLA encloses th6 Lunar 14odule. Adapter panels which enclose
the Lunar Module are Jettisoned prior to docking and Lunar Module extraction.
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