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DATED 26 July 74 January 19, 1976 -- t·· '5, PRJGRA"'1 TITLE ALSEP - PRD

ITEM NO. 6. PROGRAM NO. N/A 1. REVISION NO.

2 10. REVISION NOTES

This document is the official media for the identification of NASA ALSEP support requirements. Additions, deletions or changes to support requirements for the ALSEP program shall be made by revision to this document.

Revision 2 consists primarily of the deletion of the Particles and Fields Subsatellite (P&FS) support requirements, updates the list of supporting sites and includes provisions for use of recertified magnetic tapes for ALSEP.

Additionally, this revision hiis been prepared under guidelines of the Universal Documentation System (UDS) as defined in the Range Commanders Council (RCC) Document 501-70, Vol 2, Because of similiarity of forms and content of this Program Requirements Document (PRD) and the previous (but now obsolete) Program Support Requirements Document (PSRD), users will have no difficulty in identifying support requirements or determining the changes that have been made in this :revision and transition to current forms and directives.

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11. SIGNA"TURI!' ·~~ SIGNATURE I 13 .. SIGNATURE ~ .... SIGNATURE

I\ =-----.//lTD . E~~~ 1/ ~~..._..).... b~ G·M·~

·_) -----[~~ f't..IN,Y 'J. L• h E.A. ~. Deputy Director ~ Gerald M, Truszynski "11. . .....-~~ tions_ Integration Branch

l_tlme;-c, Stok s, Jr., l<>f"

G ound Data Systems Division Lunar & Planetary Programs Associate Administrator for

D ~-2.2..-{{p

"·;;?y~ Wilbert F. Eichelman, Chief Science Requirements Branch

OATE

UOS FORM R 102 JULY 70

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DATI!:

't. CLASSIFICATION

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UDS FORM R 101 JULY 70

L, W. Croom

Keith Kundel

James R. Bates

Mike Ward

J. Mitrano

F. Kieth

ADDRESSEE

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Added 1020 .1 ~. DATE

DATED January 19_1_ 1976 ITEM NO. 6. PROGRAM NO. N/A 7. Rt::VI SION NO. 2

13. ADDRESS

Johnson Space Center National Aeronautics and Space Administration Houston, Texas 77058

Johnson Space Center National Aeronautics and Space Administration Houston, Texas 77058

Johnson Space Center National Aeronautics and Space Administration Houston, Texas 77058

Johnson Space Center National Aeronautics and Space Administration ~uston, Texas 77058

Johnson Space Center National Aeronautics and Space Administration Houston, Texas 77058

Goddard Space Flight Center Bldg 16, Room S25 Greenbelt, Maryland 20771

U rJ CLASS I F IE D

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UDS FORM R 103 JULY 70

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INDEX OF UDS FORMS AND DOCUMENT OUTLINE :_ ·:.... -~ -;

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R 101) tOlD APPROVAL AUTHORITY

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SYSTEM SECURITY CLASSIFICATION

R 1:..1'; Ill$_. SYSTEM SCCURITV CLASSIFICATION MATH II<

R t<.'9 1056 SECURITY AUTHORIZATION

R G/ 1060 PREF~CE

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R G/ 1061 ITEM NUMBER DEFINITION

R 111 106.4 K£V TECHNICAL. PERSONNEL

R 1t 1015 TECHNICAL REFERENCES

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X R G/ 1110 EXPERIMENTS DESCRIPTION

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R 113 112.0

R 114 1125

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R 116 1140 TEST PROGRAM OPERATIONS

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R G/ U50 -OPERATING DESCRIPTION

R 127 lUI -CHARACTERISTICS R G/ 1500

R 128 lo45Z -RECEIVED DATA CHARACTERISTICS R 135 1510

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R G/ U5.t - ANTENNA SYSTEMS

R G/ u's -DIAGRAM

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R G/ 1460 -OPERATING DESCRIPTION

R 1!11 IA61 -CHARACTERISTICS

R G/ 146Z -ANTENNA SVSTEMS

R U% 1463 -FORMAT DESCRIPTION

SPACECRAFT /PAYLOAD TELEVISION

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R G/ 1465 -OPERATING OESCR IPTION

R Ul U66 -CHARACTERISTICS

R G/ U67 - ANTENNA SYSTEMS

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I. CLASS.IFICATjON

~--·---- ... , .. 2. HCPLACES f'-AGE (5) 31. PAC..l" t.IU.

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5. PR::>GRAM TITLE

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R 2.18 Z310 - CONTROL

R G/ 2.32.0 - DESTRUCT

R G/ 2330 - UP-DATA LINK

H G/ 2.3 .. 0 - UP-DATA LINK RECORDINGS

R Ul 2.360 - UP-DATA LINK STATIONS COVERAGE

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R Gl 2540 - ANALOG STR JP CHART RECORDING FORMAT

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I I. CLA$Sif--ICATION

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January 19, 1976

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R G/ 2610 - DATA

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R G/ 2700

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R G/ .)010 -FLIGHT CONTROL./SUPPORT CENTERS

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R 300 3031 -DISPLAYS

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R 3D~ 30!13 -CONSOLE ANALOG RECOHOEHS

R G/ 30!14 - CONSOLE DRAWINGS

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R G/ )040 - DATA FORMATS -GENERAL

R G/ )041 - TRACKING DATA FORMAT CONTROL.

fi G/ lOA% - TELE....;ETRV DATA FORMAT CONTROL.

R 305 3043 - TELEMETRY DATA FORMATS - DETAIL

R G/ .IOAA - COMMAND DATA FORMAT CONTROL

R G/ 30 .. 5 - REMOTE SITE DATA PROCESSING

R G/ )050 - DATA TESTING

R G/ 3060 -DATA INTERFACES

R 306 3061 - DATA INTERFACE CRITERIA

PHOTOGRAPHIC

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R 307 3110 - OET AIL

R G/ 3ZOO

R G/ 3ZIO

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R G/ 3300

R 311 3310

R 31Z 33%0

R 313 3330

R 31A 33•0

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RECOVERY

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R 317 3At1 - SEACHAF"T

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MEDICAL

MEDICAL

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R >Z' 3505 - 810-SCIENC~

R 32.J 3510 - PERS.ONNEL- ACTIVE

R3Z 3520 - PERSONNEL .- STANDBY

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PUBLIC AFFAIRS

PUOUC AFFAIR!:i St:::HVICES

R G/ 3600 - GENERAL

R .,2.5 1610 - PERSON,.._EL ASSIGNMENTS

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1. CLASSIFJCA"l ION U f.1 C I. A 5 S I f I F 0 r--------------------------------;lr-----------,----·------·----·--·

(PAGE TITLE) Z REPLACI:...S PAGE (5) .J. PAGf:. NV.

INDEX OF UDS FORMS AND DOCUMENT OUTLINE. . Added

1040

•

5

.(. DATE DATED January 19, 1976

s. ~R:JGRAM TITLE ALSEP - PRD

10.. u. tZ. USEC FORM PAGE

13. TITLE

X

NO. NO.

CAT£GORY 4 COORDINAT£ SYSTC:MS/

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CATEGORY 5 BASE FACILITIES/LOGISTICS

PAGE 5000 TO 5999

PERSONNEL ASSIGNMENT SCHEDULES

R G/ 5100 -GENERAL

R 500 5110 - O£T AIL

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UOS FORM R I 05 JULY 70

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R 501 5360 - SEACRAFT

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R 511 5600

R 512 5610

R 5tl 562.0

R G/ 6000

R 60C 6010

R 601 602D

MAINTENANCE

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FACILITIES

FACILITIES

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CATEGORY 6 OTHER SUPPORT PAGE 6000 TO 6999

OTHER SUPPORT

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REQUIREMENTS FOR SUPPORT AGENCIES

1. CLASSIFiCATION

(PAGE TITLE)

1060.1 Z. Ht:PLACES P.-.GE (S)

Added '· PAG£. NO.

PREFACE .C. OATE January 19, 1976 OAT£0

ITEM NO.

T1X T 9.TEST CODE 7. HEVI51UN NO. 2 6. PROGRAM NO. N/A 5. PR:lGRAM TITLE

ALSEP - PRD 10.

DISCUSSION •

TEST CODE DEFINITION (Box 9 of each ALSEP PRD page)

Test Codes are not used. This document reflects information relative only to the program level of support. Fut~e documents that require specific tests or operations will reflect definitive Test Codes to be used as required.

UDS FORM R G/C JULY 70

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ITEM NUMBER DEFINITION oAn:.o •- DATE January 19, 1976 I

, •• ~~M NO. ,9.TEST CODE ,_ PR:lGRAM TITLE ALSEP - PRD 6. PHOGAAM NO. 1. REV I ~I UN NO.

N/A 10.

ITEM NUMBER DEFINITION

ITEM NUMBER

The Item Number provides requirements identification and location, Entered in box 8 of each page of this document is an Item Number containing four or more elements:

1. A code identifying the requesting agency. 2. An enumeration of separate statements within a page or group of pages, 3. A test phase designator code, 4, A code identifying the support agency(s).

Requesting Agency/Number/Phase Designator/Supporting Agency(s)

Exception: Statements containing background or information items which do not require support consist of three elements, ending with 11X11 :

1. A code identifying the initiating agency, 2, An enumeration of the statements, 3. An 11X11 denoting information,

Initiating Agency/Number/Information Designator

AGENCY DESIGNATOR

The designators for the Requesting and Supporting_' Agencies are:

G - Goddard Space Flight Center (GSFC) T - Johnson Space Center (JSC)

2 --- --1

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ITEM NUMBER DEFINITION Added 1----------------,

... OATE 6 I DA.ll:.O January 19, 197

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16. ITifM NO •. J 9.TEST COOE 5. PR:>GRAM TITLE ALSEP - PRD 6. PHOGRAM NO. 7. Rt::VJ!iiON NO.

2 T2X \Cont 1 d~ N/A ~------------------------------------~------~-------~~--------------~--------------------

IC. ITEM NUMBER DEFINITION (cont•d)

NUMBERING SYSTEM

The numbering scheme for the digit portion of the item number is: The Item Number is assigned sequentially within organizational sections. Numbers added take the next consecutive number (T4, T5, T6, etc) throughout each numbered section regardless of forms used (2000.1 may begin with item T1 and continue incrementing thru 2000.8 with page 2100.1 beginning again with item T1, T2, etc throug~out the 2100 section). Inserted items between existing item numbers will use the decimal system (T4.1 after an existing item T4, etc). Further insertions will appear as next dec~l level (T4.1.1 after an existing T4.1, etc). Exception: Item numbers in the communications sections 2730 and 2760 will be consecutive beginning with T1 on each page throughout either section.

TEST PHASE DESIGNATIONS

The designators used to :i.rlentify test or mission phases are:

AP - All t>hases D.P - '"nna.r l'arkioe; Urbi t

SUPPORT AGENCIES

DS - Lunar Surface Operations NP - No Phase or Not Applicable

The letters following the phase designators identifies the agency(s) requested to provide the support for the particular requirements item. The agency indicated first is designated as the one principally responsible for the overall support system planning and, therefore, responsible for defining, coordinating, and integrating the support activities of the two (or more) agencies; subsequent designations identify the agency(s) providing or operating the detailed support systems who is responsible for detail system planning within the areas of its support responsibilities. Support documentation from each agency providing support is required to be submitted to the requesting agency.

UDS fORM R G/C

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1. CLASSIFICATION

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TECHNICAL REFERENCES 5. PR::>GRAM TITLE

... REFERENCE:

A. ITEM B.. PAGE

1.

2.

3.

UDS FORM R 112 JULY 70

ALSEP - PRD

"· TITLE

Universal Documentation System Document 501-70 (501-67 Revised) Volume 2

Network Operations Sup~ort Plan for ALqEP/P&FS (Revision 1) STDN NO, 601/ALSEP/P&FS

Data Acquisition Plan, ALSEP, Rev 1 Annex B-1: Combined ALSEP Telemetry Data Format Control Book

Annex C-2: ALSEP /P&FS Command Format Control Book

Annex E: Remote Site Data Processing Program Requirements Vol. 5, ALSEP/P&FS

Annex F; MCC/STDN Validation Testing and Support Manual

z. REPLACES PAG£ (~) ). PAGE NO. I 065,1

Added DATED

6. PROGRAM NO.

tz. PUBLISHER AND DATE:

Inter-Range Documentation Group, Range Commanders Council October, 1970

Goddard Space Flight Center Greenbelt, Maryland August 1974

Johnson Space Center Houston, TX October, 1974

July 1972

April 1972

February 1972

N/A ... Commander U.S. Army

4. DATE

January 19, 1976 7. REVISION NO. 2

SOURCE

White Sands Missile Range ATTN: STEWS - NR - P White Sands Missile Range, NM 88002.

NASA Goddard Space Flight Center Attn: Code 851.1 Greenbelt, Md, 20771

Johnson Space Center National Aeronautics and Space Administration, Code FS4 Houston, TX 77058

1. CLASSIFICATION

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1100.1 1100.1 PROGRAM DESCRIPTION - GENERAL

D"TLD 7 May 73 .. OAlC

January 19, 1976

5. PHJGRAM TITLE: , .. ITEM NO. ,9.TEST CODE 6. PHOGRAM NO. N/A 7. H£Vl51()N NO.

ALSEP - PRD T1X 2 .....-.-...-...... ,.

to. INTRODUCTION

The Apollo Lunar Surface Experiments Package (ALSEP) consists of a number of experiments which were deployed on the lunar surface during Apollo lunar landings. These experiments are used to investigate and determine the composition and structure of the lunar surface and interior, and to investigate the lunar environment.

Each ALSEP is a self-contained unit designed to transmit lunar geophysical information to earth via S-band frequencies for the lifetime of the unit. The unit consists of power supply, central station, and various experiments.

The following table discloses Apollo mission . i dates for convenience in relating ALSEP to Apollo:

APOLLQ MISSION 11 12 15 16 14** 17 Launch Da!;e 16 Jul 69 14 Nov 69 26 Jul 71 16 Apr 72 31 Jan 71 7 Dec 72

Launch Vehicle AS-506 AS-507 AS-510 AS-511 ~

AS-509 AS-512

Flight Article *EASEP 1 2 3 4 5

ALSEP Array A A-2 D c E

P&FS 1* 2*

* = Currently Inoperative ** = No uplink command capability

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1110.1 Added EXPERIMENTS DESCRIPTION 4. OATE

January 19, 1976 DATED

5. PR::>GRAM TITLE I"· TEST CODE , •• PROGRAM NO. N/A 7. HEVISION NO. , 2 ALSEP - PRD ..

ITEM NO. to. DESCRIPTION

~--------_,The original issue and rev1s1on 1 of the ALSEP/P&FS PSRD described the ALSEP experiments on pages 1130.1 th~ough 1130.7.

T1DSX

To comply with the UDS numbering system, these experiments now appear in the 1110 series. The Revision Control page will show the 1130 series deleted and the 1110 series added, with changes to the basic information indicated by an 11R11 in the right margin.

The Apollo Lunar Surface Experiments Package (ALSEP) is an experiment designed to investigate and determine the composition and structure of the lunar surface and interior; and to investigate the lunar enviornment. Each ALSEP package is self­contained and is designed to transmit 1U:nar geophysical information to earth via S-band frequencies for'periods of approx­imately two years. Current lifetime estimates are indefinite. The Unified S-band (USB) stations will receive, record and command to ALSEP as well as transmit data in real-time to JSC.

UDS FORM R G/B JULY 70 I UfKlASSifiED

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EXPERIMENTS DESCRIPl'ION Added 1110.2 <4. OA.TE January 19, 1976 DATED

I"· TEST CODE '· PR:>GRA""' TITLE 6. PROGRAM NO. N/A 1. HE\/ISION N0.2 ALSEP - PRD .. 10• DESCRIPriON (cant' d)

ITEM NO.

T2DSX The experiments associated with ALSEP are given below in accordance with ALSEP Flight Article assignments:

ALSEP Flight Article

1 2 3 4 5 A~-507 AS-510 AS-511 AS-509 AS-512

Array A Array A-2 Array D Array C Array E Apollo 12 Apollo 15 Apollo 16 Apollo 14 Apollo 17

1. Passive Seismic Experiment X X X X 2. Active Seismic Experiment (ASE) X **X 3. Lunar Surface Magnetometer (LSM) *X *X X 4. Solar Wind Spectrometer (SWS) 1{ *Y 5. Suprathermal Ion Detector/Cold Cathode X ~ X *X

Gauge Experiments (SIDE/CCGE) (See Note 1 ) 6. Heat Flow Experiment (HFE) .X *X X 7. Charged Particle Lunar Environment **X

Experiment (CPLEE) 8. Dust Thermal, and Radiation Engineering y y y

9. Measurement Packates (DTREM)(LDDE; Apollo 12) Lunar Ejecta and Meteorite Experiment (LEAM) _X_

10. Lunar Seismic Profiling Experiment (LSP) _X

11. Lunar Surface Gravimeter (LSG) X

12. Lunar Atmosphere Composite Experiment (LACE) or _X

Lunar Mass Spectrometer (LMS) * = No longer operational ** = Currently inoperative due to loss of uplink

Each ALSEP can transmit PCM TLM in a normal or contingency data rate as follows: NORMAL: 1060 bits/second; 10 bits/war~; 64 words/frame; 640 bits/frame Note 1: The CCGE on ALSEP 1 & 2

CONTINGENCY: 530 bits/second; 10 bitsVword; 64 words/frame; 640 bits/frame

UDS FORM R G/B JULY 70

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1°;: 1976 ·1 ~·-·_P_R_~_G_H_A_M __ T,IT_L __ E::~~~~~---------------------------------------------~1L~--~-----T_~_s_T_~_O_·_O_EJI_•_·_P_R_O_G_.R_A __ M_N_O __ • ____________ _l'_·_'_'_E_V_I~_-,_o_N __ N_0_._2~----~---------·~

EXPERIMENTS DESCRIPTION 4. DATE

Added

•• ITO:M ""'· ••• DESCH.IP'£ION

T2DSX (cont 1d)

T3DSX

T4DSX

The active Seismic experiment data is transmitted in the following mode: 10,600 bits/second; 20 bits/word; 32 words/frame; 640 bits/frame

The Lunar Seismic Profiling experiment data is transmitted in the following mode: 3533.3 bits/second; 30 bits/vJOrd 20 words/frame; 18\>0 bits/frame.

EXPERIMENTS

Passive Seismic Experiment (PSE)

The passive seismic experiment uses one vertical short-period element and three orthogonal long-period elements to measure the natural seismicity of the moon, the lunar free oscillations, and the tidal deformations. The data from this experiment will help determine the strain regime and energy of the moon's interior, the overall elastie properties, and the correlation between seismic sources and visible surface features.

Active Seismic Experiment (ASE)

The primary purpose of the active seismic experiment (ASE) was to generate and monitor artificial seismic waves in the 3 to 250 Hz range, in the lunar surface and near subsurface. The ASE can also be used to monitor natural seismic waves in the same frequency range. The objective of these functions is to acquire information to enable determination of the physical properties of lunar surface and near subsurface materials. Seismic waves were artificially produced by explosive devices, and detected by monitoring instruments. The resulting data was telemetered to Earth for study and interpretation. By varying the location and magnitude of the explosions with respect to the detectors, penetration of the seismic waves to depths of approximately 500 feet could be achieved, and wave velocities through several layers of subsurface materials investigated. The velocities of compressional waves, their frequency spectra, and rate of attenuation are functions of the physical constants of the near surface lunar material. Interpretation of this data permits the type and character of the lunar material to be inferred, as well as the degree of induration and bearing strength of these materials. five mortar ~ charges remain on the lunar surface (4 on A-14 and 1 on A-16). Although there are no plans to detonate these charg·"s at present, the option to monitor natural scientific phenomena still exists.

~~~~~------------------·----------------------------------------------~ UOS FORM R G/B JULY 70

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EXPERIMENTS DESCRIPTION Added 1110.4

- ···-·---~

r-----------------------------1 Z. REPLACES PAGE (S) 3. PAGE: NO. (PACa: TITLE)

OAT EO •· DATE January 19, 1976 j ~ •. --P-R-~G--RA __ M_T--IT_L_E-------------------------------------------------------~,.-.-T-E_S_T_C_O_O_E-1-.-_-P_R_O_G_R_A_M--NO--.-N-/-A---------+-7.--R-EV_I_S_I_O_N_N_0_.~2--~-------------~ ALSEP - PRD

a. ITEM NOa

T5DSX

T6DSX

T7DSX

••· DESCRIPTION

Lunar Surface Magnetometer (LSM)

The lunar surface magnetometer uses three flux-gate sensors on the ends of 3-foot booms to measure the tem1'oral variations of the local magnetic field vector. When operating in a special site-survey mode, the sensors are rotated in order to measure the local magnetic gradient and to detect anomalies such as buried iron-composition rocks. The normal mode provides data on the interaction between the solar wind and the moon's magnetic field, the moon's gross electrical diffusivity, and the structure of the earth's magnetic tail at 240,000 miles. Data from this experiment will help resolve the fundamental questions of whether or not the moon has a molten core. (The Apollo 12 and 15 LSM 1 s were commanded off on 14 June 74.)

Solar Wind Spectrometer (SWS)

The solar wind is a flow of electrons, protons, and other charged particles from the sun into space. The instrument is essentially a spectrometer and uses seven Faraday cup sensors arra~ged in a hemispherical array to determine the temporal arrl directional variations of charged-particle flux at the lunar surface. The data from this experiment will provide information concerning the interaction between. the moon and the solar wind, the moonls gross electrical conductivity, the presence of a lunar atmosphere, the effects of radiation on the surface through the mechanisms of sputtering and charging, and the earths magnetic field effects at 240,000 miles. (The Apollo 15 SWS was commanded off on 14 June 74.)

Suprathermal Ion Detector Experiment (SIDE)/Cold Cathode Gauge Experiment (CCGE)

The SIDE provides data pertaining to the density and the temperature of the lunar ionosphere as it exists near the lunar surface. SIDE meas1u·ements include ion counts as well as measurement of the velocity and the energy associated with the detected particles. These measurements are made using a low-energy particle sensor which has a velocity filter composed of crossed electric and magnetic fields followed by a low-energy curved plate analyzer. The velocity filter passes ions with proper velocities and the low-energy curved plate analyzer passes ions with the proper energy. The particles that pass through t~e curved plat~ analyzer are detected and counted. The velocity filter selects ions with velocities ranging from 4 x 10 to 9.35 x 10 em/sec. The low-energy curved plate analyzer covers an energy range of 0.2 to 48.6 ev. The experiment also contains a high-energy curved plate analyzer without a velocity filter that detects and counts solar wind particles in the range of 10 to 3500 ev.

UDS FORM R G/B JULY 70 UNCL1SSIFIED I. CLA$S!FlCATION

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1110.5 r-------------------·-1 EXPERIMENTS DESCRIPTION

DATED

Added ... DATE

January 1'), 1976 5. PRJGRA....., TITLE , •• TEST CODE, •• PHOGHAM NO. N/A 1. Ht:VlSJON NO. ~2

.. ITEM NO.

T7DSX (cont 1d)

T8DSX

T9DSX

ALSEP - PRD

1o. DESCRIPTION

The CCGE determines the neutral particle density at the lunar surface and any variations in that density associated with solar activity. Specifically, the CCGE measures the pressure of the ambient lunar atmosphere. The Cold Cathode Ion Guage groduces an electrical current that is proportional to the measured pressure over the desired pressure range of 10- torr to 10-12 torr.

Heat. Flow Experiment (HFE)

The heat flow experiment (HFE) measures the net outward flux of heat from the Moon's interior. A measurement of lunar heat flux provides information on:

A. A comparison of the radioactive content of the Moon's interior and the Earth's mantle B. The thermal history of the Moon C. The lunar temperature versus cle1i"t1 profile D. The value of thermal parameters in the first three meters of the Moon's crust

The technique used in the HFE is to measure the temperature of the moon ~ a function of the depth and to determine the steady state vertical temperature gradient. When combined with seismic measurements, data from the HFE experiment will provide information on the coinposition and physical state of the Moon's interior.

Charged Particle Lunar Environment Experiment (CPLEE)

The charged particle lunar environment experiment (CPLEE) measures the energy distribution, time variations, and direction of proton and electron fluxes at the lunar surface. The results of these measurements will provide information on a variety of particle phenomena. The CPLEE measures the energy of protons and electrons separately, and measrlres each at 18 different energy intervals. The CPLEE is capable of measuring particles with energies ranging from 40 ev to 100 kev, and with flux levels of about 105 to 101° particles per square centimeter/second/steradian • The CPLEE measures particles and therefore characteristics of the following solar radiation phenomena:

A. Solar wind electrons and protons (50 kev to 5 kev) B. Thermalized solar wind electrons and protons (50 ev to 10 kev) C. Magnetospheric tail particles (50 ev to 100 kev) D. Low-energy solar cosmic rays (10 ev to 100 kev)

UOS FORM R G/8 JULY 10 U rl CLASS f f l f n

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(PAG.£ TITLE) Z. HEPLACES PAGE (S)

EXPERIMENTS DESCRIPI'ION Added

T10DSX Dust, Thermal and Radiation Engineering Measurement (DTREM) & Lunar Dust Detector (LDDE)

T11DSX

T12DSX

The Apollo 12 Dust Detector (LDDE) was designed to collect data for the assessment of dust accretion and the measurement of thermal surface degradation.

The Apollo 14 and 15 Dust Deteq~ors had modified Dust Detector hardware and were subsequently known as the Dust, Thermal, and Radiation Engineering Measurements (DTREM) packages designed to obtain data not only for the assossment of dust accretion, but also lunar radiation and lunar surface brightness temperature.

i

The experiments measure the rate of dust accumulation on the ALSEP package. These data permit an evaluation of the rate of degradation of thermal surfaces exposed to lunar dust. The dust detectors are tltree photo cells located on three sides of the ALSEP control station. As the dust accumulates on the photo cells surface the solar radiation measured by the cells decrease§ furnishing a standard which can be used for analysis of system(s) deterioration,

The DTREM sensor package, which mounts on the Central Station sunshield, contains three solar cells 1 centimenter by 2 centimeters in size, located on the top horizontal surface. A temperature sensor is attached to the underside of the center solar cell, and two others are attached to the inside and outside, respectively, of the side of the package. The sensor pack­age is connected through an H-film cable to a printed-circuit board located in the Central Station.

Lunar Ejecta and Meteorite (LEAM)

The LEAM experiment is designed to measure the physical parameters of primary cosmic dust encountering the lunar surface and secondary spray particles (or lunar ejecta) emanating from the site of meteorite impacts on the lunar surface.

Lunar Seismic Profiling (LSP)

The L1tnar Seismic Profiling Experiment (LSP) was to artifically induce seismic energy signals to obtain data on the physical properties of the lunar surface and near-surface materials. Seismic energy generated by detonation of the remotely deployed Explosive Packages was detected by four geophones, processed by the LSP electronics and transmitted to earth via the control station. However, no further ca~ability exists to generate stesmic phenomena due to all explosive paekages having been detonated. The currently passive LPP still retains the capability to monitor natural phenomena through four deployed geophones. I

UDS FORM R G/B JULY 10 UNCI.ASSlflf.D

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~:-:-~-:-:-:-~-N_o_. __ 1_1_1_o_._

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January 19, 19?6 ~----------------------------------------------·----------r-~--------~,--------------------T-----------~~~~------1

(PA<iE TITLE)

EXPERIMENTS DESCRIPTION DATED

Z. Hi::PLACES PAGE (5)

Added

~·· __ P_R_~_G_R_A_M __ T~IT_L_E ____ A_LS __ E_P __ -__ P_RD __________________________________________ ~·-·-T_E_S_T __ CO_O_E~-·-·-P_R_O_G_R_A_M __ N_O_._N_/~A--------~-'· __ R_E_V_IS_I_O_N_N_0_. ___ 1 ______________ ,, .. ITEM NO.

T13DSX

T14IJSX

T15DPX

T16

so. DESCRIPTION

Lunar Atmospheric Composition Experiment (LACE) formerly Lunar Mass Spectrometer (LMS)

The LACE (LMS) obtains data on the composition of the lunar ambient atmosphere at the lunar surface and detects transient changes in this atmosphere due to venting'of gases from the lunar surface or from man-made sources. The LMS operates within the 1 to 110 amu mass range at the lunar surface. The instrument is a magentic sector field mass spectrometer with a Nier-type thermionic electronic bombardment ion source.

Lunar Surface Gravimeter (LSG) i

The Lunar Surface Gravimeter Experiment objectives are to utilize the moon as a space antenna to search for gravitational radiation from cosmic sources, to measure the lunar surface deformation associated with tidal forces, to provide vertica.l axis seismic activity information and to measure the ratio of lunar 11 g11 to earth 11 g11 •

PARTICLES AND FIELDS SUBSATELLITE (P&FS)

The Particles and Fields Subsatellite was used for obtaining data relati;e to the investigation of two fundamental problems of space physics: The formation and dynamics of the Earth's magnetosphere and the boundry layer of the solar wind as it flows over the moon. In addition, the P&F subsatellite provided the cgpability of obtaining precise phase-locked two way doppler measurements for analysis of the lunar gravitational field. The P&FS has been inoperative for the past several years. Attempts to command it were discontinued after the last attempts in the fall of 1974.

DELETED

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5. PRJGRAM TITLE

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T2DSX

T3DSX

T4DSX

T5DSX

T6Dsx;

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UDS FORt~ R 120 JULY 70

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10. FREQUENCY 11.

EMISSION A. a. CHAR ACT XMITTEO REC

MHz Ml:!z PSK/FM/FM 2119 PCM/PSK

PM

2278.5 PCM/PM

2278.0 PCM/PM

~CM/PM 2276.0

2279.5 r~PM 2275.5 rCM/PM

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1405.1 7 May 1973

.. DATE OAT EO January 19, 1976

6. PROGRAM NO. N/A 7. HE VISION NU. 2 IZ. 13. ... 15. 16.

GUARD PURPOSE

BAND TIME LOCATION REMARK~

-·

-

Receive Uplink data from s Scl -Lunar Earth (ALSEP) dulec Surface

Transmit TLM Data ALSEP #1 !Conti Mtflt§'ce to Earth nuous

Transmit TLM Data ALSEP #2 Conti Lunar to Earth nuous Surface

Transmit TLM Data ALSEP #3 Conti Lunar to Earth nuous Surface

Transmit TLM Data ALSEP #4 ~Conti Lunar I to Earth nuous Surface I

'Transmit TLM Data ALSEP #5 Conti Lunar to Earth

I nuous Surface

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1456.1 ~---------------------4 VEHICLE COMPOSITE SYSTEMS -OPERATING MODES Added •· DATE January 19, 1976 DATED

5. PR:»GRA'wt TtTL.E , •• ITEM NO. I .. TEST CODE •• PROGRAM NO. I '· REVISION NO. ~ ALSEP - PRD T1DSX N A ~

10. The Original issue of the ALSEP/P&FS PSRD described the operating modes on page 1455.1. To comply with the UDS numbering system, this description has been moved to page 1456.1; therefore, the Revision Control page will show page 1455.1 deleted and page 1456.1 added, with changes to the basic information indicated by an "R" in the right margin.

STDN TO ALSEP S-BAND UPLINK MODE - 2119.0 MHz

Signal Combination

16

Information

Updata

Modulation Technigue

PSK/PM

Peak Carrier Deviation Vehicle

J,r:Jf, Rad. +10% ALSEP -3%

ALSEP TO STDN S-HAND SIGNAL COMBINATIONS - (VARIES BETWEEN 2275,0 - 2280,0 MHz) '

1 530 BPS TLM PM 1.25 Rad. ±5% ALSEP 'lit

2 1060 BPS TLM PM 1.25 Rad. ±5% ALSEP 3 10.6 KBPS TLM PM 1.25 Rad. ±5% ALSEP 4 3.533 KBPS TLM PM 1.25 Rad. ±5% ALSEP

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TELEMETRY - DA -II\ GENERAL Added DATf.O •· DATE January 19, 1976

2 5. PR~GRAM TITLE I e. ITEM NO. 19.TEST COD£

T1DSG 6. PROGRAM NO. 7. REVISION NO. N/A ALSEP - PRD

10.

The original issue of the ALSEP/P&FS PSRD described the ALSEP Telemetry Tape Recording Formats on page 2215.1. To comply with the UDS numbering system, this information now appears on page 2200.1. The Revision Control page will show page 2215.1 deleted and page 2200,1 added, wit.h changes to the basic information indicated with an 11R11 in the right margin.

ALSEP TELEMETRY TAPE RECORDING FORMATS

1. Gent'lral

a, Tape recording speed will be 3-3/4 IPS· b. Recording mode, Wideband FM (28.125 KHz± 30%) c. Tape reels used for telemetry magnetic tapes will not exceed 14 inches d. HBR Support: ASE (only) recording speed will be 7i IPS e. 7 track, i" tape width will be used. 111 tape may be used as a contingency backup.

2. Timing

a. NASA 36 bit time code on 1 KHz b. SDT (Serial Decimal Time) on 1 KHz c. 6.25 KHz or 12.5 KHz speed lock is required,

3. Magnetic Tape Quantities and Logistics

a. Magnetic tape recordings are required at each station (See 4200.1, T1, for data handling procedures) b. The data will be recorded on wideband magnetic tape and will contain the following data:

(1) Command (composite data) Verification Receiver (2) 6.25 KHz or 12.5 KHz speed lock (3) Voice annotation (4) ALSEP Data FM Wideband (5) Timing

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OTHER SYSTEMS- GENERAL 26oo.1 r----2_60_0_·1 ___ ._1

~--------------------------------------------------------------------.-----------+-o-A_r_E_o _____ 2_6_J_u_l __ 7_4~------~·-·_o_A_T_E __ J_a_n_ua __ r~y __ 1_9~, __ 1_9_7_6 _______ 1 I"· TEST CODE I•· PROGRAM NO. N/A 5. PR'JGRAM TITLE 7. HEVISION NO.

.. ITEM NO.

T1DSG

T2DSX

T3DSG

ALSEP - PRD 2 . .. The STDN is required to simultaneously support all active ALSEP packages deployed on the lunar surface, Scheduling of individual STDN stations will consider the following: (1) ALSEP life expectancy is another 3 to 4 years. The support period will be extended as necessary. (2) During periods of HDR ASE telemetry, an 85 foot station or a cooled paramp 30 foot station is required for support.

~he following STDN stations are required to support the ALSEP program as scheduled: ACN, AGO, BDA, GDS, GWM, HAW, MAD, ~IL, ORR, QUI, ROS, ULA and VAN.

bELETED

REAL TIME SUPPORT

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a. Periodic MCC and STDN support is required. This support will be for approximately 2 hr/day for the ALSEP paclages; two to '•R four support periods of 4 hours duration are required each month. I~ general, the specific period is not critical,

T4DSG

T5DSG

however, several support periods each month are critical. ~

~· Continuous MCC and STDN coverage may be required to support specific tests. R

RECEIVE AND RECORD

Continuous magnetic tape recordings of all ALSEP data is required from at least one STDN site for the life-time of each ALSEP, In the event of station contingency, a nominal down-time for repair (2 hours) is acceptable except during a critical period, If a longer down-time is expected, a second site is required to be scheduled for coverage.

Commanding "OFF" any ALSEP central statioJ;J. or experiment to result in permanent termination of that central station or experiment requires prior approval of the Director of Lunar and Planetary Programs, NASA Headquarters, Code SL.

UDS FORM R G/B JULY 70

I. CLA~~JFICATION

I. CLA5!>1FICATION

(PAG& TITLE) Z. HEPLAC€~ PAG£ (S)

_._ ..... _, ..• , ... ~·

J

GRO IJND COMMUNICATIGNS- GENERAL 3. PAGI:: NO.

2700.1 ' 2700.1 I DATED 7 May 73

... OATC

January 19, 1976 I '5. PAJGHAM TITLE 1·· T£ST COD£ ALSEP - PHD

6. PROGRAM NO. N/A 7. REVISION NO. 2

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8. , .. ITEM NO.

T1APG COMMUNICATIONS REQUIREMENTS

MCC to GSFC

*1 - Duplex High Speed Data Circuit, TLM and CMD 2 - Duplex Voice 1 - Duplex Teletype, 100 WPM

GSFC to STDN (A22licable Sites) I *1 - Duplex High Speed Data Circuit, TLM and CMD 1 - Duplex Voice 1 - Duplex Teletype, 100 WPM

•. * ALSEP requires restoration if the primary circuit fails

UDS FORM R G/B JULY 70

I. CLA~~IFICATION

I. CLASSIFICATION

(PAGl TI7LE)

GROUND COMMUNICATIONS- TERMINATIONS

5. PR:>GRAM TITL.E ALSEP - PRD

.. , .. 0. II II •

lTEM NO~ CAP. ~~~

IZ.

Communications Coordination {Comm Coord)

JSC

T1APX I T l NETWORK CONFERENCE JSC

T3APX I T

UDS FORt·1 R 230 JULY 70

I

MCC

MCC for dist.

I. CL.ASSIFICATION

2760 2760.1 I . 2. REPLACES PAGE {S)

-·-· _.J::. DATE 1976 D,..TC:O 7 May 73 J&.nuary 19, ,9. TC.:ST CODE 6. Pl;rOGH'AM NO.

N/A ,7. REVISION t<C.

2 , .. - g~ l ITEM NO. CAP~ SE£ NOTE ----------

GSFC

l T2APG T GSFC Communications Manager

GSFC ~-

T4APG T GSFC, Bldg 14, NOCC

T5APG T SCAMA Switchboard, for extension to STDN sites

-UtJCLASS.!f....:....;;I[...:;:_D _

,, 'I

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:1

t. CLASSlF ICATJON UNCLASSifiED -------------------------------------------------r-----~~~----,~~~-----------z. REPLACES PAGE (S) l. PAC.&::. NO. (PAG~ TITLE)

DATA FORMATS- GENERAL 3040.1 Added

DATED •· D"-TE January 19, 1976

5. PR:lGRAM TITLE 19. TEST CODE 6. PROGRAM NO. N/A

7. AEVI!)ION NO. ~

2 .. ITEM NO.

T1DSG

T2DSG

T3DSG

ALSEP - PRD . .. The original issue and Revision 1 of the ALSEP/P&FS PSRD contained "Flight Operations - Data Processing Computer Requirements - Miscellaneous" on pages 3075.1 and 3075.2. To comply with the DDS numbering system, this iiif'ormation is now contained on pages 3040.1 and 3040.2 "Data Formats, General". The Revision Control page will show pages 3075.1 and 3075.2 deleted; 3040.1 and 3040.2 added with changes to the basic information indicated by an "R" in the right margin.

DATA PROCESSING AND RECORDING REQUIREMEJNTS

Provisions are required at the remote sites for bulk magnetic tape recordings of all ALSEP data. Recording of all active ALSEP downlinks simultaneously and corresponding time correlation is required at supporting sites. The capability of correlating the ALSEP tape record with station operating parameters is also required.

All USB sites are required to format any two of the ALSEP downlinks and to transmit this data to MCC. All combinations of live and playback date are required; i.e., two live, one live and one playback, or two playback. This requirement applies to any site receiving ALSEP data transmitted in either the normal or contingency mode. Reference should be made to the ALSEP Telemetry Data Format Control Book (DAP Annex B-1) and ALSEf Remote Sites Data Processing Program Requirements (DAP Annex E-1) for specific format details. Data processing will be accomplished by a telemetry and command progra1n which will be loaded in a single 642B computer.

When ALSEP #3 (Apollo 16), #4 (Apollo 14) or #5 (Apollo 17) rudLV, in the High Bit Mode, only that vuhiclets data is required lfi to be processed, formatted, and transmitted to MCC by a particular site. Another site may be simultaneously receiving one of the other ALSEP downlinks and transmitting its data to MCC. The total data rate transmitted from a site to MCC shall not exceed 2.4 KBS of the 7.2 KBS data line.

One program within a single 642B computer will handle both telemetry and command processing. The command portion of the program must receive command information from the MCC or station CAM and process and transmit these commands to the ALSEP packages. Uplinked commands will consist of 75 bits transmitted most significant bit first and formatted as follows:

Preamble 20 bits (all ones) Decoder address 7 bits Command complement 7 bits Command 7 bits Timin<T 11.. hits (all ones)

UDS FORM R G/B JULY 70 UNCI.ASS I FlED

I. CLA~'SJFICATION

t. CLA: '•II IC.~l ION

DATA FORMATS - GENERAL l ~-:-;~~ci4o~2- - -- .. --~--

., "· 0"' L January 19, 1 ')76 -----·-

Z. HEf~LACI:..S t,AGL (~~)

ADDED

OAT EO

(PAGIL TITLE)

'· PR:JGRAM TITLE ALSEP - PRD ~ •· TEST coac I•· PRO<>HANI NO. NA I 1. ncv1 "'"'"' Nu. 2 f----"-'"'!r--______________________ _._ ____ ....._ _________ -"----------- ------·

8. 10 • . ITEM NO.

T3DSG (cont•d)

T4

T5DSG

The maximum number of ALSEP commands that may be designated is 128 per ALSEP package. Reference should be made to ALSEP Data Formats Contra~ Book for specific details concerning the experiments command formats.

DELETED

ALSEP SPECIAL SUPPORT REQUIREMENTs

JSC requires special support of t~e active seismic experiment from the STDN 85 foot stations and the cooled 30 foot paramp stations. These stations must be'capable of receiving a downlinked bit rate of 10.6 KBS, processing selected parameters, and packing the data into a HSD format for the real time transmission to MCC, A special support period occurs near the end of experiment operation.

ALSEP -Pass Summary messages are required to .be transmitted via Teletype to MCC following each support period of the STDN stations. The ALSEP Pass Summary Messages will include USB receiver signal strength in DBM at (1) AOS elevation angle, (2) Max elevation angle and (3) LOS elevation angle.

The dual USB stations are required to support both ALSEP and other missions simultaneously when requested by MCC. System #1 will be configured for ALSEP support and system #2 for other assigned tasks, Tne ALSEP data will be transmitted to MCC via one high speed data circuit,

UDS FORM R G/B JULY 10 UNCLASSIFIED

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1. CLA~SIFICATION UNCLASSIFIED ----------------------------------------.-~--·--------.---------------·--· I

Z. REPLACES PAG£ (S)

~3---P_A_G_E_"_N_0_._4_2_o_o_._1 _____________ 1 DATED 7 May 73 •- DATE January 19, 1976 I

1----------------..---+------"-----t-----=--___:__---, !•· TEST CODE •• PROGRAM NO. N/A

~------r-------------------------------------~------~~----------~--~-------------------·

(PAG£ TITLE)

- Dl $POSITION - GENERAL

2

FLIGHT EVALUATION DATA 4200.1

'· PRJGRAM TITLE 7, REVISION NO,

ALSEP - PRD .. 10. ITEM NO.

TELEMETRY MAGNETIC TAPE HANDLING

T1DSG ALSEP magnetic tapes recorded during a scheduled support period on any given day, will be held on station for 24 hours after the final LOS of that day, for possible playback. After 24 hours, the tapes will be shipped as follows:

DR

T2DPG

TJAPG

All stations (except ACN) making shipments that require customs clearance will ship tapes via airfreight to GSFC/Code 864.2 Shipments will be weekly e~cept during special support.

All stations making shipments not requiring customs clearance will ship directly to JSC using either of the following methods, except for special,!support:

a. Ship via airfreight once per week. b. Ship via the U.S. Postal Service, registered air mail, daily.

ACN will ship "tapes via Eastern Test Range (ETR) aircraft to Patrick AFB, Florida.

During special support periods tapes will be shipped by airfreight C4PN via ETR) on the next available flight, or as specified by ISI.

GSFC will forward all magnetic tapes to JSC.

DELETED

DELETED

UOS FORM R G/B JULY 70 IHH:tASS I FlED

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I. CLASSIFICATION

(PAG!i: T JTLE) Z. RL:PLACES PAGE (S) 3. PAC.C r-.o. --~~

Janoory 19, 1976 -~ ~--------------------------------------------------------------------~~~~~~~+-------------------------~----~~~~~~~~--------~

DAT£0

4200.2 Added •. DATE:

'· PR':JGRAM TITLE 9. TEST CODE 6. PHOGHAM NO. N/A 1. REVISION NO. 2

~------~-------A~L~S~E~P~~P@~----------------------------~--------~------------------~~------------------·---· .. ITEM NO.

T4APG

tO.

RECERTIFIED MAGNETIC TAPES FOR ALSEP

In support of the ALSEP data processing requirements, the GSFC through its magnetic tape recertification facility, will provide JSC the necessary number of recertified digital computer tapes to be used in the ALSEP bulk data processing. This will allow used magnetic tapes of sufficient quality to be obtained through an internal NASA source at less expense than procuri~g new tapes. Coordination of this task will be through JSC, Code TN 3.

Tapes no longer required at JSC will be turned back to the GSFC tape lab for reuse.

UOS FORM R G/8 JULY 70

I. CLASI5JFICATtON I

UfiCl ~ \\lflfD I i I

NASA-JSC