LSG 770-154-10 - LM-5 LUNAR MODULE STRUCTURES...
Transcript of LSG 770-154-10 - LM-5 LUNAR MODULE STRUCTURES...
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Prepared By:
LSG 770-154-10 - LM-5
LUNAR MODULE
STRUCTURE S
HANDOUT
LM-5
FOR TRAINING PURPOSE S ONLY; IN SUPPORT OF LM -5 STRUCTURES COURSE
FOR
FLIGHT CONTROL DIVISION
AT
MSC, HOUSTON, TEXAS
Approved By:
/V, if&wiu_y£� \ William Strasburge IM Instructor
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)
TABLE OF CONTENTS ( Cont)
·ChaP,�er 2 Iunar Surface Equipment Deployment
Equipment Locations - Descent Stage
Modularized Equipment Stowage Assembly (MESA)
MESA Deployment Back�p Deployment MESA Deployed MESA Deployment Mechanism MESA Deployment Ratchet/Spring Assembly Modularized Equipment Stowage Assembly MESA Ballet MESA Ballet with Equipment MESA Stowage List - IM-5 MESA Side Views MESA Pallet W/0 Equipment TV Camera and Tripod Closeup Stereo Camera - Stowed Lunar Stereo Camera Tongs Gnomon Hammer w/Extension Handle Scoop Solar Wind Composition Experiment
S-Band Erectable Antenna
S-Band Deployment Sequence S-Band Erectable Antenna Handling S-Band Erectable Antenna
Early Apollo Scientific Equipment Payload (EASEP)
EASEP Deployment Sequence (1, 2, 3, 4) Scientific Equipment Bay Door
Lunar Samples
Frame & Cable Assembly Deployment Mechanism
Sample Return Box Scale Lunar Equipment Conveyor
IM-5
� 2-1
2-2 2-3 2-4 2-5 2-6 2-7 2-8 2-9 2-10 2-ll 2-12 2-13 2-14 2-15 2-16 2-17 2-18 --2-19
2-20 2-21 2-22
2-23 thru 2-26
2-27 2-28
2-29 2-30 2-31
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Chapter 1
)
TABLE OF CONTENTS
Ascent and Descent Stage Structure
IM Ianding Gear
IB.nding Gear Primary Strut
Ianding Gear Secondary Strut
Landing Gear Deployment and Downlock Mechanism
Stowed Position Down and Locked Position
Translunar Flight
CSM Separation from LM & SIVB
Post Transposition Docking
LM/CSM Undocking
Thermal Control
Typical Thermal Shield and Blanket
Thermal Control Coating
Blanket.Joining
Abrasion Protection and Penetration Insulation
Standoff Installation & Blanket Venting
Panel Shingling - Front View
Bay Vent
Landing Gear Thermal Protection
Micro-meteoroid Protection
RCS Plume Deflector
Descent Stage Base Heat Shield
Temperature Graphs
EVA Antenna Erection Mechanism (l) EVA Antenna Er ection Mechanism (2)
IM-5
� 1-1
1-2
1-3
1-4
1-5. l-6
1-7
1-8
1-9
1-10
1-11 � 1-12 .. :.· . .... ... <
1-13 --
1-14
1-15
1-16
1-17
1-18
1-19
l-20
l-21
1-�"�2
1-23
1-24
l-25
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CABIN SKIN ASSEMBLY
��
l: .. ASSEMBLY
· SPECIMEN RETURN ', CONTAINER
:·• ASSEMBLY
MID SECTION ASSEMBLY
UPPER DECK � ASSEMBLY
.� SCIENTIFIC EQUIPMENT BAY
LOWER DECK ASSEMBLY
I 'ASCENT AND DESCENT STAGE STRUCTURE T30915-83.1
IM-5
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DEPLOYMENT TRUSS
'•:
OUTRIGGER
---,6 .. __ ----,2 .. __
LANDING
I L:!�;: LANDING GEAR I
PRIMARY STRUT
CROSS-OVER TRUSS A SSY.
SECONDARY_. STRUT
k--------36�"--�-----T30900-99.3
-
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)
) -
BEFORE IMPACT
4500#
OUTER --------CYLINDER
10 IN.
INNER CYLINDER
HONEYCOMB CARTRIDGE
9500#
STROKE (COMPRESSION)
AFTER IMPACT
321N.
I LANDING GEAR PRIMARY STRUT I T30005-213
LM-5
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DOWN
)- CRANK ASSEMBLY----------
·.LANDING GEAR DEPLOYMENT AND_ . N; LOCK,•MECH�NISM· QvJ;EO POSITIONl..'
�DESCENT STAGE
DEPLOYMENT TRUSS
LM-5
T30915-18.2
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LOCK ROLLER TRUSS�
TRUSS SUPPORT LINK
DEP LOYMENT TRUSS A SSEMBLY
LANDING GEAR DEPLOYMENT AN D
DOWN LOCK MECHANISM (DOWN AND
LOCKED POSIT ION )
LM-5
ISUAL INO ICATOR
•
T30915-19.2
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X
ROTATION 1.5 TO 2.5 RPH
20° OR LESS
I TRANSLUNAR FLIGHT I
SOLAR INPUT
T30005-201.1
IM-5
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! INBOARD
PLUME
(HEAT RATE a TIME)
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ALUMINUM STRUCTURAL SKIN
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DOWNLOCK DEPLOYMENT MECHANISM
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TITANIUM GUARD PLATE
PAINT
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PRIMARY STRUT
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NUMBER OF FOILS ( INCONEL SKIN/NICKEL FOIL 8 MESH)
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.�'.' .. :
H.;.FILM BLANKET (1/2 MIL, 25 LAYERS)
ENGINE NOZZLE EXTENSION
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v
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-FILM BLANKET (1/2 MIL, 25 LAYERS)
SUP
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TITANIUM BACKFACE STRUCTURE
H-FILM BLANKET (112MIL,I L
10 LAYERS
3 LAYERS
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r DESCENT STAGE BASE HEAT sHIELD 1 T30005-196.2 §2
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ANTENNA ERECTION MECHANISM' ( 1) I T30715-142
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EQUIPMENT STOWAGE ASSEMBLY MESA PALLET
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Weight Earth Illnar D!J./CSM Item Lbs. Qty Launch Launch Transfer
Lunar Television Subsystem Lunar Television Camera 7-2 l * TV Wide Angle Lens .4 1 * TV Lunar Day Lens .4 1 * TV Cable Assembly (100 ft) 2.4 1 * TV Tripod Assembly 1.74 l *
Equipment Lunar Transfer Bag l *
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Lunar Sample Scoop ·9 l *
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Sample Return Container #l 15.6 l * * * Scale l Solar Wind Composition Bag 1 Sample Bags 5 Packing Material Bulk Sample Container l
Sample Return Container #2 20.9 l * * * Solar Wind Composition Bag l Core Tubes 2 Documentation Sample Collection Bag l Sample Bags 15 Gas Analysis Container l Lunar Environment Sample Container l Packing Material
Date: May 1969 Page 2-9 ··-FoR-TRAINING PURPOSES ONDY
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Date: May 1969 I ;\ { ', I'
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[SCIENTIFIC EQUIPMENT BAY DOOR FRAME 8 CABLE ASSEMBLY
Date: May 1969 Page 2-27 PURPOSES ONLY
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SCIENTIFIC EQUIPMENT BAY DOO DEPLOYMENT MECHANISM
Date: May 1969
T30005-232
Page 2-28
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