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NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
APOllO 15
FINAL
LUNAR SURFACE TELEVISIONOPERATIONS PLAN
JUlY 5, 1971
PREPARED BY
APOLLO COMMUN (CATION SYSTEMS SECTION
FLIGHT CONTROL OPERATIONS BRANCH
FLIGHT CONTROL DIVISION
MANNED SPACECRAFT CENTERHOUSTON.TEXAS
SUBMITTED BY:
APOLLO 15LUNAR SURFACE TELEVISION
OPERATIONS PLAH
(FINAL EDITION)JULY 5. 1971
•APOLLO COMMUNICATIONS SYSTEMS SECTION
~/Z::~/toWARD I. FEHDEL(HEAD, APOLLO COMMUNICATIONS SYSTEHS
SECTION
APPROVED BY:
CONCURRED BY:
#DIRECTOR:
11
FLIGHT CREW OPERATIONS
•
APOLLO 15
LUNAR SURFACE TELEVISION
OPERATIONS PLAN
(FINAL EDITION)
PREFACE
This document has been prepared by the Apollo Communication Systems
Section. Flight Control Operations Branch, Flight Control Divsiion.
Manned Spacecraft Center, HOllston, Texas. The information contained
within this document represents Lunar Surface Television require
ments and planned operations for Apollo 15. Mission J-l as of
July 5. 1911.
Any questions or comments concerning this document should be directed
to FC2/G. A. Pennington, Flight Control Operations Branch, Apollo
Communications Systems Section, at area code 713. 483-2267.
This document is not to be reproduced without the written approval
of the Chief, Flight Control Division. Manned Spacecraft Center,
Houston. Texas.
iii
May 2008 Publication Note
The Apollo 15 Final Lunar Surface Television Operations Plan was the document prepared for use during the Apollo 15 lunar stay. It provides reference material for those who need addi-tional information about the operation of the Lunar Rover color television camera during Apollo 15. It was published on July 5, 1971, by Manned Spacecraft Center. The original document was provided by Dick Nafzger, who was the Manned Space Flight Network television engineer at Goddard Space Flight Center during the Apollo missions. This PDF version was produced by Bill Wood. The original pages were scanned with an Epson Expression 10000XL, using Silverfast AI Studio, to produce high quality 300 pixel per inch, 48-bit images, for further processing. Each page image was straightened and cleaned up in Photoshop CS3 prior to producing 150 pixel-per-inch EPS page images. Adobe Acrobat 8 Professional was used to add the bookmarks before the final PDF edition was produced.
iv
LUNAR SURFACE TELEVISION OPERATIONS PLAN
I. INTRODUCTION
The Apollo 15 Lunar Surface Television Operations Plan is used
to document the Lunar Surf'sce TV operations plan, to provide
detailed rr:v operating procedures, and to document all Lunar
Surface TV requirements to be implemented.
This document includes detailed t imeline procedures am
operational TV requirements. Tlmelines are essentially task
nw analysis along a time base showing the points of inter
action between the two crewmen and Mee, and simply list, in
sequence of performance, the steps required to carry out each
of the tasks. It is 1n the detailed timeline procedures that
the MCC/ Crew/Equipment interfaces are revealed. The tasks of
the CDR, LMP, and MCC are presented side-by-side so that no
confusion will exist as to which party is doing what, or h~
the three cooperate in the television operations on the
lunar surface.
II. REQUIREMENTS AND PRIORITlES
The lunar surface television requirements as documented in
this publication, are considered as highly desirable and not
mandatory. The television coverage does not supersede or
delete in any way the photographic requirements specified in
the Mission Requirements Document (MRD). The following
1
•
comprises a detailed list of the Lunar Surface television
viewing requirements for the Apollo 15 mission.
A. Requirements for Individual AlSEP Experiments
1. Experiments
a. Passive Seismic (PSE)
b. Lunar Surface Magnetometer (LSM)
c. Suprathermal Ion Detector (SIDE)
d. Cold Cathode Gauge (CooE)
e. Solar Wind Spectrometer (SWE)
f. Heat Flow (HFE)
g. Central Station (CS)
2. General Requirements
a. Monitor AtSEP off loading, RTG Fuel
cask removal and RTG fueling.
b. Pan area from lock to lock (+170° to _110°)
prior to AlSEP deployment operations and after all
experiments are deployed.
c. Attempt to relate each experiment with an
identifiable nearfield object (such as another
experiment) .
d. Obtain a medium angle view of each experiment
during and after emplacement.
e. Observe general activity around each experiment.
3. Specific Reguirements
a. Central Station:
(1) Obtain a panoramic view of the deployed ALSEP
in relation to the CS.
(2) Obtain a narrow angle view of the antenna.
antenna gimbal. and interface between the
antenna gimbal and antenna mast.
2
•
b. Passive Seismic Experiment:
Obtain a close-up view of the PSE thermal shroud
contact with the lunar surface (to determine if
gaps exist).
c. Lunar Surface Magnetometer:
(1) Obtain a close-up view of the IBM sensor
heads and tripod. after deployment.
(2) Obtain a view of the L5M cable after
deployment.
d. Suprathermal Ion Detector/Cold Cathode Gauge:
(1) Obtain a close-up view showing relationship of
SIDE to eCGE.
(2) Monitor deployment to determine stability of
SIDE during deployment of SIDE and CeIG.
e. Solar Wind Spectrometer:
None except per the General Requirements section.
f. Heat Flov Experiment:
(1) Observe at close-up range, as much of the
probe hole drilling operations as possible.
(2) During drilling, observe deviation of drill
from vertical position.
(3) Observe insertion of probes in holes and
deployment of cables and electronics package.
B. Non-ALSEP Experiments
1. Experiments
a. Laser Ranging Retro Reflector (LR3)
b. Soil Mechanics Experiment
3
c. Lunar Field Geology Experiment - LM
d. Field Geology - LRV
e. other
2. Requirements
a. LR3,-(1) Pan the deployment area fran lock to lock
(+170° to _170°).
(2) Obtain a close-up view during aoo after
emplacement.
(3) Relate the LR3 vit 1 an identifiable object
such as ALSEP deployment site.
b. SoU loEchanics:
(1) View the core tube sampling operation and
penetrometer tests at each core tube site.
(2) View the trenching operation aDd pmetrcmeter
test.
(:~) View of rover wheel tracks, where poasible.
c. Field Geology - Lunar Module:
(1) Pan 3600 with horizon near top of frame and
widest field of view.
(2) Sight on LM with maximum and minimum zoan
poaitions to permit scale calibrations on
MCC SSR n/TV monitors for later traverse
measurements fran LRV.
d. Field Geology on LRV:
(1) 3600pan at all stops, wide angle, horizon
near top of frame. This should not be a
4
continuous pen, but a pen-stop, etc. Stops
should be 2-4 seconds long (for Polaroid
camera photos) and pens should have aominimum of 10 overlap.
(2) On request f'rem the Public Affairs Officer
or Experiments Officer,zoom from wide angle
to telescopic view at sampling localitiesoor local landmarks as defined f'rem the 360
pan.
(:~) During traverse, look at LRV tracks, fenders,
and vheels, at each science stop if surface
conditions deem necessarYjsuch as excessive
dust, or extreme differences in wheel penetra
tion (determined by astronaut).
(4) During traverse stop, zoom frem wide angle
to telescopic view of Lunar Medule, previous
stops am future stops.
e. Other Requirements:
(1) Establish a grid snd calibration scheme for
range and bearing determinations.
(2) View LRV deployment and equipnent stowage
on the LRV.
(3) View LRV operation during checkout peried
(especially observe braking).
5
•
(4) View ALSEP offloading from lM and deployment
in the field.
(5) View equipment jettison from LM after 3rd
EVA.
(6) View LM descent stage and ALSEP after 3rd EVA.
Details to be defined later.
(7) View LM ascent.
(8) Color survey of lunar terrain in eastern sun
light, high sun angle on August 3-5, 1971.
(9) View 1M impact.
(10) If sufficient power is available and no thermal
problems are encountered, view solar eclipse
at 13:24 p.m. CDT on August 6, 1971.
(11) Color survey of the lunar terrain in western
sunlight on August 1, 8, 1971.
III. OPERATIONAL AND EQUIPMENT CONSTRAINTS
A. The Lunar Conununications Rele;y Unit (LCRU) viII operate
in the voice/data mode only with the LRV moving. The
S-Band low-gain antenna and a MSFN 85-foot dish are
required for the moving modes. No television can be
transmitted in these modes.
B. The LRV must be stopped for transmission of television due
to S-Band antenna pointing.
Television requires the high-gain antenna and an 85-foot
or 21Q-foot dish. (See page 15, Figure 111-1 for 210 foot
site coverage).
6
C. The crewman must dismount the LRV to operate any LCRU
controls (medes, power, telemetry monitor) or to deploy
or adjust the high-gain anteooa.
D. The Extra Vehicular Suit Canmunications (Eves) can be
operated line-o:f-sight to the LCRU within 500 meters with
no degradation in VOICE or data. Degraded but usuable
voice and data may be obtained to a range of 800 meters.
E. The delay in transmission of video to MCC f'ran the lunar
surface is approximately 1.8 seconds.
F. The amount of tiTlE from the execution of Groorxl
Commanded Televis ion Assembly (GCTA) commands until
video response at MCC is 3.7 seconds maximum. (i.e .
....hen TV is received by Honeysuckle Creek, Australia and
transmitted to MCC via satellite).
IV. TELEVISION Monn>
A. General
The Color Televis ion Camera (CTV) has several different
mcxies of operation. At the beginning of Lunar Surface
operations, the CTV is mounted on the MESA and video is
transmitted via the LM - 100 foot cable and S-Band system
7
to the }'sFN'. This is the same configuration of the
television camera as used on previous missions. Shortly
after MESA deploy and the first video is transmitted fran
the MESA, the crew will mount the r:I!V on a tripc:d to view
LRV (Lunar Rover) deploy aal MESA off-loading. The MCC
has no canmand capability while the r:I!V is connected to
the m via the lOO-foot video cable.
After the Lunar Canmunication Relay Unit (LCRU) and
Television Control Unit (TCU) are ofnoaded and mounted on
the LRV, the crv is turned off, disconnected fran LM
power, and mounted on the Tal (ref figure IV-l). After
LCRU mc:de checks are made the crv will be activated in
the LCRU "TV RMI"1 mc:de. Fran this point on, video will
be transmitted to the MSFN via the LCRU.
B. Specific Modes
The "TV RMT" and nFM/TV" modes of the LCRU are used for
transmission of television. The "FM/TV" mcde downlinks
1.25 MHz voice, PLSS data, LCRtJ data and video to the MSFN
on S-Band. Control of the Ground Canmand Television
Assembly is exercised manually by the crew or by ground
canmand frcm the MCC in this mcde.
8
The "FM/TV" mote 'Will be used for naninal television
operations during the traverses.
The "TV RMrIt mote of the LCRU has the same capabilities
as the "FM/TV't merle but has the additional capability
to turn off the LCRU 1.25 MHZ VOICE/DATA subcarrier
and power down the LCRU FM/PM transmitter. Due to the
capability to turn off the 1.25 MH VOICE/DATAzsubcarrier, the ttTV RMrtt mooe can downlink video only
with an increase in video quality. The "TV RMrtl merle
'Will be used to view ALSEP deploy and activities within
the VHF raDge of the LM where additional television
quality is desired and LCRU voice snd data are not
needed. The capability to turn off the LCRU FM trans
mitter will be used post-EVA 3 to save power for
further r:YV operations.
V. INCO INTERFACES AND PROCEDURES
The Instrumentation and Communication System Officer (INCO) is
responsible for ground commanding the GCTA and implementation
of the Lunar Surface Television Requirements. During real
time mission operations, the INCa will receive additional
inputs on operation of the GCTA from the Experiments Officer
(EO), TV Support Bldg. 440, and the Flight Director. In
addition, the Public Affairs Officer (PAO) will make inputs
to the Flight Director who will pass the coordinated
input to INCa. The EO is responsible for taking
9
inputs fran the lunar field geology Principal Investigators
(PI) and relaying them to INCO. The type of inputs expected
in real time operations are as follows:
a. Narrow-Angle Targets of Opportunity (NATO) of specific
geological formations viewed. during the wide-angle
panorama (WAF) at the beginning of a traverse stop.
b. certain cre\l activity not scheduled for television
coverage.
VI. SPECIFIC !NCO PROCEIXJRES
A. Wide-Angle Panorama (WAF) - The WAF vill occur \lhen the
Lc:fW/Gf!rA 1s sw1tched to the "FM/TV" mode at the
beginning of each traverse stop. It vill consists of 14
discrete pans of 24° each with stops after each pan of
4 secome duration. The minimum time to accanp11sh a
WAF is approximately 168 secome. The WAF vUl start
fran :;1700 and end at the opposite stop. The starting
point is determined by the position of the r:I!V at the ti~
of activa.tion.
B. Narrow-Angle Target of Opportunity (NATO) - The NATO is
accomplished by centering the desired object
in the television picture vith the zoan at minimum
(12.5 tam). The centering may require canb1na.tions of pan
and tilt. When the object is centered in the field-of
view (FOV) of the CTV t the CTV will be zoom.ed in to the
maximum zoom position (75 mm).
10
C. Medium-Angle View (MAV) - The MAV is accomplished by
positioning the object/area to be viewed in the center of
the television picture with the zoom at medium (-30 mm).
The MAV will be used when the area around an object is
of interest for determining placement or general
activity.
D. Typical Traverse Stop Activation - After the CDR dismounts
the LRV, he will switch the LCRU to the trFM/TV" mode,
which applies power to the GcrA, and point the LCRU High
Gain Antenna (HGA) to earth. In addition, if this is a
stop within LM VHF range and the LCRU was not previously
powered up, the CDR would be required to place the LCRU
paver switch to "INI'".
E. Use of the LCRU "TV RMI''' merle - The LCRU "TV RMI''' merle will
be used during ALSEP deploy and around the LM where voice
and data need not be traosmitted from the LCRU. The
"TV RMl''' merle will be used instead of the ItFM/TV" merle
when the capability of being able to turn off the LCRU
1.25 MHz VOICE/DATA SUBCARRIER and improve the television
picture quality is desirable. Additionally, the 'tTM RMI'lt
merle wlll be used for viewing LM ascent.
For the LM ascent canmand sequence to work the LRV/LCRU/o
GCTA must be positioned 180 frem the LM Ascent Launch
Azimuth at 328 feet from the IM. Nominally the
LRV will be driven along the derived bearing until the
11
•
odometer clicks .1 km (328 feet). The crewman will then
point the LRVon a bearing of 255°. The LeRU will be
act!vated on "EXT" power in the !lTV RMT" mode and the
LeRU HGA pointed toward the earth.
The MeC will then command the CTV so it is pointing at the
LM. If it is impossible to position the LRV as required
due to a large crater, rock, etc., the LRV will be
positioned to the north of the proposed site. The new
position will require azimuth correction commends to be
added to the ascent command sequence. The nominal ascent
command sequence is defined in the detailed timeline.
Section IX. page 45.
F. Use of LRV Power - The LCRU has the capability to use LRV
paver in addi ticD to the LeRU internal battery. This
capability will be used for covereage of 1M ascent and it
will also provide additional power to increase LCRU/GCTA
post-ascent operations time. To use LRV pover the LCRU
pover swi tch is placed to "EXT" and the LRV power Aux
circuit breaker is closed.
G. CTV Traverse Stowage - Prior to departure from the Lunar
Module or a science stop, the CTV will be positioned by
ground command or manually by the crew to !1700 in Azimuth
and _45 0 in elevation. This CTV position is desirable
from an operational and thermal standpoint. Operationally
the stowed position will save time in positioning the CTV
for a Wide Angle Panorama and also provide a known reference
fOT determination of bearing of the crew or an object from
the LRV.
12
VII.
A. GarA REMOTE CCWlAllD CONl'ROL
COMMAND
* PAN RIGHT
* PAN LEFT
FUNCTION
DRIVES CTV TO RIGHT AT 30
/SECOND
DRIVES CTV TO LEFT AT 3o/SECOND
PAN STOP
POWER ON
ALC PEAK
POWER OFF
STOPS CTV AZIMJTlI MOTION
DRIVES CTV UPWARD AT 3o/SECOND
DRIVES CTV DOWNIiAIUl AT 3°/SECOND
STOPS CTV ELEVATION MOTION
CTV ZOOM: DECREASES LENS FOCAL LENGTH
CTV ZOOM: INCREASES LENS FOCAL LENGTH
STOPS ZOOM
CTV IRIS: DECREASES LENS F/NUMBER
CTV IRIS: INCREASES LENS F/NUMBER
STOPS CTV IRIS MOTOR
PROVIlE3 LIGHT CONTROL ON "ffiAK SCENE LUMINENCE
ALC AVERAGE PROVIDES LIGHT CONTROL ON AVERAGE SCENELUMINENCE
1. PROVIDES 28 VDC TO CTV2. PROVIDES 28 VDC ON LCRU FM TRANSMI'I'rER
CONTROL LINE3. COMMANDS sic ON
1 • TURNS OFF POWER TO CTV2 • TURNS OFF POWER ON LCRU FM TRANSMITTER
CONTROL LINE
S/ C ON WRNS ON LCRU 1.25 MRz VOICE SUBCARRIER
sic OFF WRNS OFF LCRU 1.25 MRz VOICE SUBCARRIER
* THESE COMMANDS JlAVE ASSOCIATED INCREMENT COMMANDS.
* Z()Ct.{ OUT
* ZOOM IN
ZOOM STOP
* IRIS OPEN
* IRIS CLOSE
IRIS STOP
* TILT DOW
TILT STOP
* TILT UP
13
B. COOMAND TYPES
1. Type I Ccmmand
Single function RTC (e.g. pan right) at delay fran RTC
ioitiate until function start 1.9 seconds.
2. Type II Ccmnand (1Dcre~Dt)
Dual fU.nction RTC (e.g. pan right at, paD stop, pan stop).
Two single function RTC's um.er one FBI vith a built in
wait perted between commaoos.
NOl'E:THE LAST CCf.IMAND IS EXECl1l'ED TWICE
PAN RIGHT AT PAN STOP PAN STOP
_75 M,S'-4 75 M.S._ +-75 M.S.-.
14
1000 M.S. ~1-65 M.S. 1lFUNCTION FUNCTION FUNCTIONINITIATE INITIATE INITIATE
14
SiTE 210'COVERAGE SS' ---- --- ----- ----------- ---- --- •• ---- ---- ---- :s_
1&\ lb2 ~~ l&i los 1\ 0 JIl2 d4 1\ 6 lis 1~0
UNOOCK POI TO to
-.- " " .... .. .. .. .. .. .. .. .. ." "'."'."' -: ..
. - r :s -------- • • •:s --z • • • ++ - E E =- .. , .S& •
1~0 1 1~2 1~4 lh lIs1
1'30r
d2 d4 ,lS6 ds
i1~0
EVA 1 I
w •
1~S
.. .. .. .. .. .. .. .. .. .. .. ..
---- • ---- •* • -= •• - -- --
llO I1142
1 I1\6
,,4s 1
ltO144, EVA 2 ,•• r, -- -
" ..
.w.i i
160
............... - - " :."..:....... ..-..
&: --- . ------------- _.--- ---- - --- .- -. r-- - - -_.-I I I I I I I
~2 OO~l4i
~I
160 162 164 166 168 170 176 180I EVA·) I C r
•
VIII. The following pages are a detailed timeline of Lunar
Surface Television operation versus crew activities time.
16
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orr • lCRU or: • TV RJn • GOA OFr IASSiSt CIll: STOll CIll', I'lSS .wn:-. Id(SS
I I- I,ClOSE Iti\TCH REPRE5S W'II
,!
1os .. 00,4S
END [VA. THm5TtICI'O 0lI21A
•
IX. LIFT-OFF AND POST-LIFT-OFF LCRU/GCTA OPERATION
A. General Description
At the end of EVA III, the LRVjLCRU/GCTA will be positioned
180° from the ascent launch azimuth (276 0) at a range of 0.1
kilometer (328 feet) to view ascent with the color television
camera (eTV). The LRV will be pointed at a bearing of 255°.The CTV will be ground commanded according to a predetermined
command sequence to follow the ascent stage (page 46).
Post-Lift-Off operation of the LCRU/GCTA from August 2-8,
1971, at the Hadley Rille site will serve five purposes as
follows:
(1) Coverage of the 1M ascent stage lift-off and initial
trajectory
(2) Survey of plume effects near the landing site and on
the descent stage
(3) Coverage of an eclipse of the sun by the earth on
August 6, 1911
(4) Survey of lunar landscape colors and albedo \Ulder
changing S\Ul angles
(5) Observations of planets, stars, nebulae, and other
astronomical objects
A complete schedule of camera operations is given in the
detailed timeline section IX, B. Camera geometry is
presented in Figure IX-l. The post-lift-off operations
as presented in the detailed timeline will be accomplished
based on LRV battery power remaining and thermal considera
tions. All post EVA III activities are time referenced in
GMT rather than GET (Ground Elapsed Time) due to the pos
sibility of GET updates during the mission. GET reference
is provided as a flight plan reference only.
B. DETAIU:D TIME LINE
1lJ\.'.l't; ·t'.lj:;~lT-(:-i') ::UN TJ\.TiCl::1'7r.crli Cl'f;{Wl'lON ~-~i_'_"i':'~'i;v·---'i' -
-};f.JW ---;'\: -, --- ".. '11H:~1HI: f,!':C I,m!!:. ~'!'. '!{TI1, \
AU<. 2 16: 110:00 ,,0 115° MCC·COIJJ[DlI.m pO\ler on 4,% 27°5 MAD 2(171:06:00 GET\ Read out LCRU volt8@:e,
racliator telllperature aDdcrv tel'lperature
16:42:00 4,° 115° HCO - C_"" 1.25 MHZ sub- 47°E 27°5 ,carrier off, position cry toviell LM ascent
1(,:45:00 4,° 115° MCC - Monitor crv until 470" 27°5 20ascent
Ascent Command Sequence---17:11:24 4,° 115° MCC cOOllllSDd: TILT UP 47
0E 27°5 2
(171:37:24 GET)17:11:26 MCC Call1l8nd: ZOOM OUT
17:11:]4 HCC camnaDd : ZOOM STOP
17:11:36 HCC ccums.Dd. : ZOOM IN
17:11:42 HCC ccmnaDd. : TILT STOP
17:11:43 HCO cCtQlll8Dd : TILT INC DOOm , ,17:11:45 NCC command: " TILT INC OOWN
17:11:47 HCC commaDd. : TILT INC DOWN
17:11:49 HCC commar:d : TILT INC DOWN
17:11:51 HCC command : TILT INC DOWN
17:13:24 4,° 115° MA.V surface/1M. descent stag 46°E 27°5 ,for plume effects
17:16:24 4,° 115° Pan hor1zon, MAV 460" 27°5 ,17:19:24 4,° 115° HCO - CalIlI80d POIIer ott 450" 27°5
I
46
DATE THIE·-(j:;"rrT 'UII TARGET/GCIA OPERATION SUB-LUNAR SITE T liTHR:MlN:SEC ELEV AZ LONG. LAT. (MIN. )
Aug 2 17:52:00 ",0 115° MCC - Command Power ON 41° E 17° s MAO 2
{Cont (172:18:00 GET) view Earth, AZ 190° El. 600
17:54:00 430 115° View Saturn, 2° East ot 41° E 27° S 2
Earth
17:56:00 440 116° View Milky Way, 25° West of 40° E 27° s 2
Earth
17:58:00 W 116° Pan Horizon, MAV 400 E ,,0 , 3
18:01:00 440 116° Point CTV for Thermal 400 E ,,0 , 1
Management
18:02:00 440 116° MCC _ Command POWER OFF 39° E 27° S
22:00:00 MCC - Command POWER ON, 1.2 2
(176:26:00 GET) MHz Subcarrier ON, andread out LCRU voltage, LCRUradiator temperature, andCTV temperature
22:02:00 MCC - Command 1.25 MHZSubcarrier OFF, POWER OFF
Aug 00:51:00 4,0 119° MCC _ Command POWER ON, GO' ,(179:17:00 GET) position CTV tor LM Impact
01:05:00 450 119° View LM Impact - NATO ,Impact area, read out LCRUVoltage, LCRU radiatorte:mperature, and CTV te:mperature
~
It LM Impact reQ.uirement isdeleted, add TV/LCRU on torgeology.
01:10:00 450 119° MCC _ Co=mand 1.25 MHzSubcarrier OFF, POWER OFF
07:00:00 470 121° MCC _ Command POWER ON, 2
(185:26:00 GET 1.25 MHz Subcarrier ON, andread out LCRU voltage, LCRUradiator temperature, andCTV t_perature
47
DA'l'E TiI·:;E:\GI.ff/ SUN TARGET GCTA OPERATION SUB-LUNAR SITE orHR:MIN:SEC ELEV AZ 1.OIlG. LAT. (MIll. )
A"" 3 01:02:00 470 1210 MCC - COlIlIlland 1. 25 MHZ(Cont) SUbcarr1er OFF, POWER OFF
13:00:00 MCC - Command POWER ON, 1.25 HSK 2<l91:26:oo GET) MHz SUbcarr1er ON, and read
out LCRU Voltage, Rad1atorTemperature, and CTV Temperature.
13:02:00 NCC - Canmand 1. 25 MHz HSKSubearrier OFF and POWER OFF
20:00:00 NCe - Command POWER ON, 1.25 MAD 2(198:26:00 GET) MHz Subearr1er ON, and read
out LCRU Voltage, Rad1atorTemperature, and CTV Temperature.
20:02:00 NCC - COIlIIIIand 1.25 MHz Sub-earrier OFF and POWER OFF. MAD
"" 4 02:00:00 ,40 1510 NeC - Command PO'rIEIl ON, 1.25 GDS 2(204:26:00 GET) MHz Subearrier ON, and read
out LCRU Voltage, RadiatorTelIlperature, and CTV Temo-perature.
02:02:00 MCC - Canmand 1.25 MHz Sub-carrier OFF and POWER OFF. GDS
09:12:58 ,60 1350 NCC - COIIIIland POWER ON, view 1150 W 260 S GDS 2(211:38:58 GET) Earth A'l. 1900 EL 600
, Geology
09:15:00 W 1350 Pan Hor1zon, MAV 1150 W 26~ S 3
09:18:00 ,60 1350 NATO - Jearby erater or reek 1160 W 260 S 3tor lun aD&1e effeets
09:21:00 j60 1350 ICC _ Ce-nd 1.25 MHz Bub- 1160 'tI 260 S 2carrier OR. read out LamVoltage, LCRU Radiator T_-perature, and CTV Tellpel'atur
09:23:00 ,60 1360 NeC - POlition CTV for ther- 1110 W 260 S 1l1li.1 IIII.nagfllllent, c~d 1.25MIIz Subcarrier OFF.
48
HR:MlN:SEC
ug 4 09:24:00(Cont)
SUN TAflGET{GCTA OPERATION
/lICC - COIIIIll&nd POIolER OFF
SUB-LUllAflLONG. LAT.
1770 \l 260 s
SIT;'; tJT(MIN. )
GDS
16:00:00(218:26:00 GET)
16:02:00
ug 5 00:30:00 61° 1510
(226:56:00 GET)
MCC - COlllll&nd POWER ON. 1.25MHz Subcarrier ON. and readout LCRU Voltage. R&41a1;orTemperature, and CTV Temperature.
/lICC - C~and 1.25 MHz Subcarrier OFF and POIlER OFF
/lICC - COIIIIlIand POWER ON, 1. 25MHz Subcarrier ON. and readout LCRU Volt88e. RadiatorTemperature, and CTV Temperature.
HSK
HSK
MAD
2
2
00: 32: 00 /lICC - CCIIlIIl8.nd 1.25 MHz Subcarrier OFF and POWER OFF MAD
06:00:00 6~ 155°(232:26:00 GET)
MCC _ COlIlIIWld POIlER DB. PAN 110° W 24 0 SHORIZON, MAV
GDS 4
06:04:00
06:08:00
06:10:10
06:11:00
13:30:00(239:56:00 GET
13:32:00
NATO _ Nearby crater or rock 1100 \l 240 Stor .un angle ettect.
MCC _ COllIlI&nd 1.25 MHr. Sub- 111° \l 24° Scarrier ON. read out LCRUVoltage, LCRU Radiator Tem-perature, and CTV 'lIe111pera-ture.
I«:C _ Podtion CTV tor 1120 W 24° SThermal Man&@;ement. CaDalld1.25 MHz 6ubcarr1er OFF
MCC - C~d POWER OJ. 1.25Ml!r. SUbcarrier OB, and readout LCRU Volta&e. RadiatorTeIIlperature. and C'1'V TeIIlperature
GDS
HSK
HSK
4
2
1
2
DATE 'rUlE \ G1.fl' J BUll i'ARCE."l'/GC'I'A OPERATIO! SUB-LUNAR SITE OTKR:KIII:SEC ELEV AS LONG. LAT. (MIt!. )
A"" , 20:30:00 M:C - C~ POVER 01, 1. 25 MAIl 2(Cont (2116:56:00 GET MH:I: SUbcarrler 01. &twl read
out LCRU Voltq•• R&41atorTe.perature. UI4 crv '1'_perature
20:32:00 MCt - C~ 1.25 MHr. Sub- ,carrier OFF &lid POWER OFF
A"" 6 03:30:00 6,· 177° MCC - C~ POWE!! OJ. 1. 25 MAIl 2(253:56:00 GET) MHz SUbcarr1er OJ(. a.n4 read
out LCRU Volt.... RadiatorTemperature. and CTV '1'__perature
03:32:00 6,· 177° M::C - C~d 1.25 MHz; Sub-carrier OFF and POWER OFF MAIl
10:30:00 MCC - Ce-and POWER OJ. 1. 25 GDS 2(260:56:00 GET Mlr. Subcarrlu OJ. and read.
out LCRU Volt.... Radiator're.perature. aJl4 r:rv '1'_-perature
10:32:00 ICC - C~d 1.25 MHr. Sub--carrier 0" and POWER OFF GDS
17:58:00 6,· _165° )CC - C~ PO'oIER 01. 1. 25 93° ! 17° S PKS 2MHz Su'bcarrler 01, &D4 readout LCRU Volt... , RadiatorT.-p.rature. &lld CTV '1'_perature.
'0
DATE rUlE _.~G:",:~ SUN TARGET/GCTA OPERATION SUB-LUNAR SITE OTHR:MIN:SEC 'LEV AZ LONG. LAT. (MIn. )
Aug f, 18:00:00 6,· _166° MCC - command 1.25 lIubellTt'ie 920 E 1-7°5 PKS 1(Cont OI'F. Point CTV at Sun tor
5 sec. ZOOlIl in
18:01:00 W _166° Pan horizon, MAV 92°E 17°S 5
18:06:00 W _1660 Point CTV at Sun tor 10 sec, 9loE 17°S 1ZOCIII In.
18:07:00 W _166° Pan horizon, MAV 900 E 17°8 5
------- --- -- Repeat above sequence. 10 ae -- --- '0at Sun. 5-min pan on II. 6-mincycle.
NOTE
Thi. c1cle will be accom-pIhbed band on UIOuntof TV picture "blocmlDlj. t1
18:23:00 W _165° Point CTV at CRESCENT SUN. 85°E 11°S 2:Z:~ in (10 Bec on Sun; 10Bee ott Sun cycle tor 2 min)
18:25:00 W _165° Total eclipse. point CTV to 84°E 17°5 5(268:51:00 GET) view corona, ring, Venus
18:29:00 W _165° Point CTV to view Lunar ".. 17°S 2Module. fore,ll;round. B-SLSS(color cal)
18:31:00 W _165° Point CTV to view total 820 E 17°S 5eclipse, corona, ri~, Venus
18:36:00 6,· _165° Point CTV to viev Apennines. 81°E 17°S ,foreground. B-SISS
18:39:00 W _165° Point CTV to view eclipse, BO·E 17°S 5Zodical light. Venue
18:44:00 6,· _165° Point CTV WSW. 45° to viev 79°E 17°S ,Milky Way. 30° to Saturn
51
DATE '1'UlE_.~C:-r:! SUlI TARGET/CCTA OPERATION SUB-LID1AR SITE OTHFI:MIN:SEC ELEV AZ LONG. LAT. (MIN.)
Aug 6 18: 48: 00 63' _164° Point m to view corona, 770 E 17°S PKS 2(Cont Zodical light, Venua
18:53:00 63' 196° Pan horizon, zoom out, in; 770 E 17°5 MSK 6MAV toreground rocks mdB-SLSS, zoom in
19:01:00 6,' 196° Point CTV to view eclipse 76°E 17°S 5dug
19:06:00 63' 196° Point r::rv to view Zodiacal 74°E 17°S 5light 10° E of Earth
19:11:00 63' 196° Point r::rv to view foreground nOE 17°6 ,rocks. MAV hori zon
19:14:00 63' 196° Point r::rv to view Apennine 72°E 17°S 2Front
19:16:00 6,' 196' Point CTV to view eclipse 720 E 17°5 10ring, planetoid, Venus
19:26:00 63' 196' Zodiacal light, Venus 700 E 17°S ,19:29:00 6,' 196° Point crv to Az 220° to view 69°E 17°S 2
Saturn (30° wsw ot Earth)zoom in
19:31:00 6,' 196' Point CTV to Az 235° to view 68°E 17°S 2Mi~ Wq (45° wsw of Earth)zoom out
19:33:00 6,' 196' Point crv" to view LM Descent 68°E 17°6 HSK 4Stae;e Az 282°, zoom in
19:37:00 63' 196° Point CTV to view nearby 67°£ 17°S Trocks, craters, Az 270°,zoom in
19:44:00 63' 196' l!:clipse ring, planetoid, 65°Z 17°6 HSK 10Vema
19:54:00 63' 197° Pan horizon, zoom out and in 62.. 17°S 5
52
DATE Tn!E~_~Gf~~ SUl: TARGET/GCTA OPERATION Slffi-LUNAR SIT';:; 'THR:MIN:SEC E V AZ UlNG. LAT. (MIN. )
A"" 6 19:59:00 63" 197° Foreground roeke and ~SLSS, 61°E nOS ESK 5{Cent ZOClll in
20:04:00 63' 19'7° Eclipse ring, planetoid, 600 E 17°S 10Venus
20:14:00 63" 19'7° Zodiacal light 15° Wof Eart 57P E 17°S 10
20:24:00 63" 197° Eclipse ring, planetoid, 55°E 17°5 10Venus ESK
MAD
20:34:00 63' 197° Zodiacal light 15° E of Eart 520 E 17°5 10
20:44:00 63' 197° Eclipse ring, solar corons" 500 E 17°5 10Venus
20:54:00 63' 19'7° Foreground rocks, Apennitlel, 48°E 17°S 3B-SLSS
20:57:00 63' 198° Eclipse, Bolar corona, Venus 47°E 17°S 9
21:06:00 63' 198° Totality ends; solar crescen 45°E 16°5 1(271:32:00 GET) 10 sec
21:07:00 63" 198° Apennines, z~ in 450 E 16°8 2
21:09:00 63' 198° Pan horizon, ZOOIIl oUt and in 44°E 16°s 5
21:14:00 63' 198° Foreground rocks, zoom in 430 Z 16°8 10
21:24:00 63" 198° Point CTV to cool c~era 400 E 16°8 1
21:25:00 63' 198° Power orr 400 E 16°s MAD 0(271:51:00 GET)
A"" 03:30:00 62' _156° MCC _ eo-and POWER 01'1', 1.25 ODS 2(2'7'7:56:00 GET MHz Subcarrier Oft, and read
out LCRU Volt-.e, RadiatorTemperature, and CTVTemperature
53
DATE TIHE \Gl.frl SUII TARGET/GC'I'A OPERATION SUB-LUNAR SITE .THR:KUi:SEC ELEV AZ LONG. LAT. (MIN. )
Aug 7 03:32:00 62· _156° I«:C - COfIIIII&nd 1.25 NlIt. Sub-- 'DS 2{Cant carrier OFF and PO'IIIR 0",
10:00:00 W _1119° MCC - COllIDalld POWER ON, 1.25 142°W 14°s 2(284:26:00 GET) MHz Subcarrier ON, and read
out LCRU Voltage, RadiatorTemperature, and (!fV Te.per....M.
10:02:00 W _149° MCC - COllllIIand 1.25 MHz aub- 142°W 14°s 5carrier OJI'F and Pan Horizon,MAV
10:07:00 W _149° Point (!fV to view foreground, 143°W 14°5 10nearby rock or crater, B-SLSSand zoan in
10:17:00 W _149° Point (!fV to view Earth and 1460W 14°8 5Leo atarl (Az - 118°, EL 63°)
10:22:00 6,· _149° Pol1tion (JJ!V for thermal 141°W 14°5 1management
10:23:00 6'· _149° MCC - Command POWER 0" 141°W 14°5
16:00:00 MCC - Command POWER ON, 1.25 'SK 2(290:26:00 GET) MHz Subcarr1er ON, and read
out LCRU Vo1tae;e, RadiatorTeIIlperature, and (!fV
Temperature
16:02:00 MOC - Calmand 1. 25 MHz aub-carrier 0" and POWER OFF
Aug 8 02:00:00 MCC - Command POWER ON, 1.25 HSK 2(J00:26:oo GET) 5ubcarrier 0", and read out
LCRU Vo1t",_, RadiatorTemper.tun, and f:rVTemperature
02:02:00 MOC - C~d 1. 25 MHz aub--carrier OFF ad POWER O'P"F
5'
DATE 'rIME (G:I,'I') SUlI TARGET/GCTA OPERATION SUB-LU!IAR SITE 'THR:MlN:SEC E V .Z LONG. LAT. (MIN. )
''''' 8 05:30:00 55· _134 0 MCC - COmmand POWER ON, 1.25 GDS 2(Cont (303:56:00 GE."I') MHz Subcarrier ON, and read
out LCRU Voltage, RadiatorTemperature, and r:rvTemperature
05:32:00 55· _134 0 MCC - COmmand 1.25 MHz 8Ub- Scarrier OFF and Pan Horizon,MAV
05:37:00 55· _134 0 Point r:rv to viev foreground, 10nearby rock or crater, B--SLS •and Zoom in
05:47:00 55· ~134° Pol! tion r::rv for Thermal 1Management
05:48:00 55· _134 0 MCC - Cc;IIIIIand POWER OFF 7
06:25:00 55· _134 0 Predicted 108' of LCRUdcnml1nk due to Lunar1ibration effects on theLCRU HCA pointing (i.e.,low downlink signal strength)
55
\\
•
......'U'-Li.£I.I./fJ ",II,,
/'
-100
_roo
_300
-400
----1"".........'-'-- __ - - ,,- - +....~..,.,. "\
""~(' \~r •
•" ,,,,
•
,,,"•,
• Wr.:l. __\ \..l,DJ __---
PERSEUS(jSTARS
SATURN '"
,
LCRU,,AI!TENNA
CANis r::7IWORUSTMs
IS /CLUSTj
4 AUG)'
/_.~ .,$'
VENUS. ,,~
" ll/~::'S:: .-"(A~FIGURE IX-l. PANOO.... FOR CTV F_ LItV(328 FT EAST 01' lJ'I)
FOO POST-LIFTOFF, APOLLO 15, HADLEY RILLE(ALTITUDE PLOTTED RADIALLY.~1°. ASTRONOftICALPOSITIONS AOE FOO Ip" COT ON AUGUST 6, 1971)
~ 8AUG
\'\
~AUG
'-
,6
o -I -; -J -4 -5 -6 -7
ECLIPSE TO SUNSET 11.20
E
FIGURE IX-2, LUNAR LIBRATION - LATITUDE AND LONGITUDE OF THE
SUB-EARTH POINT AT 00:00:00 GMT ON AUGUST 2.1971 TO
AUGUST 14, 1971
7AUG l'."
6AUG2
F4 UG3
5,.•. ~- V V ,",uG4
4 DUM TER 1\ V l.o) /OF E RTH /' -3
\ V\ V II. \0 -
V/" '\ I UGG
I
\ I~~I/0
/''"-IV L'" V-2
\ V ~./,0-3
'\ V ~/G9 ............ f-..-4
-5 ~ L-:.:\ k-6 -
AU ~IL ~ ''\...-12Ai),
+6 +S +4 +3 +2 +1o
LIFTOFF TO ECLIPSE -6.3LIFT"F TO SUNSET _17,00
TOFF
57N..... _M.C_ComI.. " ......Oft. T••••
APOLLO
LSTOP
FINAL
LUNAR SURFACETELEVISION
OPERATIONS PLAN
APOLLO 15
JULY 5,1971
NASA,
FCDMSC
NASA
