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B,,,5:2f1 LAUNCH VEHICLE" '''', 

TELEMETRY AND C()MMAND SYSTEMS 

ANTI ~" DETECT~ON, ... 

RECONNAISSi~i\J E i\MERA 

MISSION CAPABlllT 

HATCH PAYLOAD RECOVERY 

Approved for Release: 2018/11/16 C05115150 
• R R. 57 ••• • • I I. iApproved for Release: 2018/11/16 C05115150 II1II 

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D-21B EMPLOYMENT 

Approved forF~·elease: 2018/11/16 C05115150 
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THE 0-218 RE CO~JNA IS SANC[ SY STEN1 I S AN A DVM'.JCE 0, S PE C! AL PUI;;POSF SYSTEM WH I ell Ci\N PROVI Df DET.A I UD 

RECONNAISSANCE COVEf,;/\GE OF HOSTILE TERRITORIES. THE SYSTFrv\ IS B;\SFD ON nn: lJNf\\!\NNlD D-,'lB HIGH P[f\FOIV.\i\\JC! 

VEHICLE WHICH IS Ali~ I.MINCHED Fl\OI\I 1\ g-5il1 !\I'~CHMT i\FHH CAI~I~Y'OUTm M..!Y lJ\ I nrS11NAflON IN THf 

NORTHERN HEMISPHEI~[ THE CAPABILITIES Of THE SY ;\i~E rOSSI!~ BY !TICA! i\\il! i\G! tH 

THE 0-218 AND THE 8-52H EXTENDED Cr\RRYOUf WITH INIlIGIIT I\UiIl!: ·A~. 

WLLOWING /\!R LAUNCH FRUM THE 8"52/1, ria 1)-2lB 1:,;\CCrlJIV\fI D iu \1;\CH~.5; !\Nt);\\.; !\1I11lHH or SO,ClOll flU BY 

A SOLI D PROPELLANT BOOSTER ROCKEr. Tilt PfNDiD BUl)5 !ll~ IS IHU\ 3fT!! >UNl!) AND THE D- B S f\ 

NAUTICAL Mill CRUISE OVFI< 1\ COURsr WHICH IS P!H-PROG!~M;\r\\tD 1\ I i\ll~T!'\1 C;UIDANC! snM. ,\rnn !\JO O! 

lHE PRE-OCTlf<l\iINED COlJI~S[!\ C(j~JTRUllJD Dl:~nNI 1\ :\\Ml! rn 1\ HH\U~ llWDI \VHIRl IHI Ht\ i CONlf\INING IHf 

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WHERE AN 1\11< I{ETI~I[V/\L !S Excel D fW JC~UOB 1\!I~Cl~MT. 

THE D .. ?.IH RFCONNf~I~;Sj\Nct S\~~lr;\1 DR/\\\/S ()\ /\ CO\S! !':i\Hll i\i\i1 lli !\i'ti?! JiCC,,\\lill\iTD UN 1m [hi, 1/, 

YF-l2A AND SI~-11 P!WGf~I\i\\S. THIS Bi\CKG!,OUND i(il\l D ,\fry 1(1 H HI! HI i PI RfO!\i\·)!\ D<:lB 

VEHICIJ t\ND TO ITS PI TO-RrCONNAISSJ\NCF l\ND i\\lH;;·\DAI< !"\1l11Iq· < 

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PROPULSION SYSTEM 

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till i~AMJFT i\UTllMATICi\\IY IGNiYrD DUfllNG 

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ALTITUDE- FT 

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RECOVERABLE HATCH 

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BOOST PHASE PERfORMANCE 

15 BOOST PHASE TRAJECTORY IS 

PRE-PROGRAMMED 1:\ THE INERTiAl 

NAVIG.AT10N SYST[M 

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APPROXIMATELY 90 SECONDS 

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• Approved for Release: 2018/11/16 C05115150 

DES C RiP 11 0 N __________________.___ .... _ .. __ 

FLIGHT DECK MODIFICA liONS '_""~"_~ __ " 

SPEED - ALTITUDE BOUNDARy ..... 

B-52H CARRY OUT PERFORMANCE __ 

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2-2 

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2-5 

2-6 
DESCRIPTIO 

"H" MODELS Of THE B 52 HAVE BUN MODIFIED 

PERFORM THE D·21B CARRYOUT ,'\ND LAUNCH MISS!ON. 

THE MODIFICATIONS CONSIST PRINCIP,Al.LY OF THE FOLLOWING: 

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\~;[) 11I.\11:';(~\:,1l 

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Approved for Release: 2018/11/16 C05115150 

FLIGHT DECK MODIFICATIONS 

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STELLAR INS RACK (0 DUAL TM RECEIVERS, l/R 

STAR TRACKER PLATFORM (]) LCO'S SEAT, LEFT HAND \..~/ 

LCO'S SEAT, RiGHT HAND CD "1 TRACK TAPE RECORDE!l 

PERiS~OPE, D,21B OBSERVATiON, L/R CD FLEXWRITER UNIT 

leo CONTROL PANELS, L/R @ FLEXWRITER DRIVER UNIT 

pproved for Release: 2018/11/16 C051151 
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Approved for Release: 2018/11/16 C05115150 

B .. 52H SPEED-ALTITUDE BOUNDARY 

MATED CONFIGURA nON 

50,000 

40,000 

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10,000 

100 

8-52 + X-IS 

140 180 220 

CALIBRATED AIRSPEED - KNOTS 

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260 300 
Approved for Release: 2018/11/16 CO~~.~~1.5_0 

B .... 52H CARRYOUT PERFORMANCE 

TYPICAL LONG RA1\'GE CAPABIUTY 

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N A V I G A TI 0 N __________ . ______ ~ ___ . __ ._. ___ . ______ ... __ . ___ .. ___ ... ____ ... _._. __ .. __ . ___ .3 - 2 

SYSTEM INTEGRATION -----------------------------.--------.-- ----.... -.. --

N A V I GAIl 0 N A lAC CUR A C Y _____ . __________ .. _____ . _____ . _____ ._________._ 

.. __ 3-3 

3-4 
NAVIGATION 

TWO SEP/\RATE INERTIAL NAVIGATION SYSTE~\S 

i\R~ PROVIDED FOR THE D-218 MISSION; ONE 

IS LOCATED IN THE B-52H FOR CARRYOUT AND 

ONE I S INSTALLED IN THE D-218 FOR THE UNMMNED FLIGHT. THESE SYSTEMS ARE ESSENTI,ALLY IDUHICAL HOWEVER THE 8-52H SYSTEM 

IS AUGMENTED BY A STAR TRACKER WHICH 

PROVIDES HIGHLY ACCURATE STELLAR POSITIONING, THE SYSTEI\\S ARE INTERCONNECTED DURING 

rv\iI,TED CARRYOUT SO THAT THE D-218 INS Ci\N 

BE UPDATED TO THE ACCURACY OF THE 8-521-1 

STELLAR INS FROM TIME TO TI~\E AND PARTICULAr~LY JUST PRIOR TO LAUNCH. 

THE B-52H NAVI GA TlON IS ,ilCCOiv\PLI SHED BY 

THE SINS PROVIDING LOCATION INFORi'v\ilTION 

FO R THE P I ~OT TO STEER BY, THE D-218 NAV 1-

GATION IS FULLY AUTOIV\i\TIC AND PREPROGRAMMED I N THE I NS COMPUTER, STEEI\! NG 

SIGNt\LS ARE SUPPLIED TO THE I\UTO!\IATI C 

FLIGHT cn"HROL ,),{SIE:"! WHI CH IN TURN 

SUPPLIL ~IGNf\L:; TO THE CO'~TROI. SURFACI: 

HYDRAULIC SERVO ACTUL\TORS, 

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SYSTEMS INTEGRATION 

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Approved for Release: 201,8(1.1./1,.? C05115150 

D-2lG If,IS f'OSlTlON EI~ROr! ACCUMULilTION 

UPDATED TO [H2H STELLilR INS PERIODI ell 

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HOURS AFTER NAViGA TlONAl ENTRY 

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B - 5 2 H A I R P l AN E IN F UGH T . _______ .... _ .. _. ____ . ___ . ___ . __ .... _. _____ 4 - 2 

DES C RIP T ION __ ._. ____ ... _ .._... .. _.......... __ ._.. ._ ... ___ .. _. __ . __ ._. ______ ._. ___ . _____ 4 - 3 

TELEMETRY SY STEM _. ____ . _____ ... _ ..... ___ . 4-4 

ANT E N N A lO CAT ION S .. __ ._... ...... _.. .. __ ...... _ ..__ .. __ . ___ . __ ..... _____ 4 - 6 

EVENTS 5 E QUE NeE __ .... _ .... ___ ._ .......... _ ... _____ . ______ . ____ ._ 4-7 
2018/11/16 C051151 
DESCRIPTION 

TELEMETRY SYSTEM 

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1.:" !u\ 

COMMAND SYSTEM 

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Approved for Release: 2018/11/16 C05115150 

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[l'll S S I ON f~A~\GE 

OFF 

TELEMETRY SYSTEM TRAN~,,\\I;> 

SPACE-POSITION AND SPEED DATI\ 

FOR L4UNCH CONTROL OFFI CER 

MONI TOR I NG DU RI NG BOOST PHASE 

AND FOR FIRST TEN MINUTES 

OF FLIGHT 
for Release: 2018/11/16 C05115 

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B~52H/Dow21B ANTENNA LOCATIONS ~ 

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_' BOOSTER IGNITION INHIBIT 

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BOOSTER IGNITION5' PITerl-UP, FULLOWED 

BY 1"IS[C PUll-UP 

TI~i\N"1 TION TO FINAL 

CliMB TRAJfCTORY 

4 M!\NLlAL DESTfIUCT 

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SEQUENCE Of EVENTS 

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Release: 2018/11/16 C0511515 

14 FUll "OFf" 

1) I.J[eT HillCl' 

16 ,41JTOMATI C DESTRUCT 

17 HIITCH RECOVERY 
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ANT I - R A DAR DES I G N ________ . _____ . __ .... ____________ ., 5 - 2 

R A DAR 5 I Z E COM PAR ISO N _._. __ .. _____ .. ________ ........... ____ ..... ___ ... _._._ 5 - 3 
Approved for Release: 2018/11/16 C05115150 

Approved for Release: 2018/11/16 C05115150 
Approved for Release: 2018/11/16 C05115150 

Approved for Release: 2018/11/16 C05115150 
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CAMERA MODES 

R E CON N A 1 S SAN C E CAM ERA CO V ERA G E____ ...... __ .~ .. -... .... 6 - 4 

FILM DATA FORMAT _ ........... __ .. _ .................... _ .... _.~ .. _ .. _._ 6-6 

H R - 335 PH 0 T 0 ____ . ____ .. __ ._ .. _. _____ . __ ..... _._._ ... _. __ .. ___ .. _ .. _._ .. _____ . ___ ._._. __ . __ 6-7 

proved for Release: 2018/11/16 C0511515 
I Approved for Release: 2018/11/16 C05115150 

CAMERA MODES 

1 [vIOuE 3 OPEfV\T10N TtJE CAi\\ERt~ PROVI DES A SVvEEP 

OF lQ DEGR~[S LEFT M,m PIGHT OF FLIGHT PATH. THI S 

SC"lEEP {MOt: Uf' OF 3 FRM,1[S PPOVI DES A LATER/IL 

COVERp,GE Of 16 Ni\UT1CAL f'{jlLES FROM THE 0-213 

CRUlc,E ,';UITUDE OF 85,000 F[ET. [(l,CH SWEEP OF 

ThE CMi:ERfi PiWVIDfS FORI'IARD OVERLAP, 

5 10 15 20 25 

D\RECTlOi~ OF 

FU GHT 

___ Approved for Release: 2018/11/16 C05115150 

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MODE 5 

I:" \VJO[ :; OPER,6,T!Oil' THE C/l,,\\[flfl PROVIDES 4 SWEEP 

OF 3·6 DEGR[ES LEFT :d~D RIGHT OF FLlGf-iT P./\Tf1, 1Hl S 

S\'iEEP iVIADE UP OF .5 FRMliES PROVIDES A L"TERilL 

COVEfUIGE OF 28 NAUTI CI\L {'iii LES FRO,'v" THE D'.zl8 

CRUISE ALTITUDE OF 85,000 FEET, E.ACH S\'~'EEP OF 

rHE eMERI\ PROViDES FORWARD OVERl;\f) , 

DfGf<FCS 

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40 

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10 15 2(1 2S 30 3> 
RECONNAISSANCE CAJ\4lERA, C 

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Fl{.~\;\"\!·S, 

EttAGE 
il\UDE 5 - lATER.';L COVERAGE 

28 N. i\\ I LE SAT 

85, 000 FEtTl\ LTITliDF 
FILM DATA fORMAT 

DATA PEIHINENT TO THE FRAMES ARE 1M/ICED ON 

EACH EXPOSURE AS /\N INTEGRAL I'ART OF THE 

PHOTO COVERAGE. DATA INCLUDES LATITUDE AND 

LONGITUDE, SIDE POINTING ANGLE (INCLUDING 

f\lflCRAFT ROLL /\NGLEl, TIME !IND FRAME NUMBER. 

THE l!'liC ERROR liNDICATES A MflLFUNCTION IN 

THE FORWARD MOTION COMPENSATION SYSTEM 

/IND OVEHflATE ERROR INDICATES THf1.T THE CAMERA 

STABILIZATION SYSTEM WAS UNABLE TO CORHECT 

FOR VEHiCLE PITCH AND ROLL. 

DMA FOR 

DI RECTI ON OF rf\ 

FI Livi TRAVEL L¥' 

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DIHECTION 

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Dlll[;:TIONOF I"l 

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FLIGHT OF D-21B SIN 505 _________ . ____ _ 

F II G H T 0 F D - 21 B S / N 51 2 .. __ __ _ 

TYPICAL MISSIONS 

6-7 
roved for Release: 2018/11/16 C051151 

fLIGHT OF D-218 SIN 505 

LAUNCHED 

MAX. MACH 

MAX. ALT. 

LAUNCH wr. 

6-16-66 

89,000 H 

7822 LB 

48 NdN. 26 SEC. 

R ll..NGE 1539 N.M. 

~,' ,-', j 

AcrU/\L RANGE 1550 N.M. 

\'\1 1 .. )'; C! 

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, , LAUNCH 

J3Z 

~ CHECK POiNTS AT ~ 

~ 50 N MILES iNTERVAL ~ , ' 'v // /.r' // '" /./ -r./ f -" /J''''''' J.t> f'.r<!' /.F' ........ ./" //// ... / "'".;. 

Fun OFF ACTUAL 

FUEL OFF 

(PLANNED) 

88 K 

130" 

~ I 

8 N. MILES ~~I " 

t 

PLANNED 

PACKAGE 

EJECT 

~ 7 N. MILES 

126" 124" 

- -- PLANNED COURSE 

--ACTUAL COURSE 

1\\:) Dcl'!\ af.XlNi!<ilTfl RlJIOOU! 

!\30AHD US\5 f~A;~G[ nU\Cr<tR /;~o 

~C-l2l i\\RC~:MTl 

1200 

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fLIGHT 0 D-21B SIN Sl 

LAUNCHED 

MAX. MACH 

MAX. ALT. 

LAUNCH WI. 

D-21B 

BOOSTER 

TOTAL 

6-16-68 

3.25 

91,700 FT 

10,746 LB 

13,119 LB 

DURAT!ON 

87 MIN. 39 SEC. 

PLANNED RANGE 2745 N.M. 

(GROUND D I STANCE) 

LAUNCH TO FUEL SHUTOFF 

32° 

30" 

26" 

24 e

, 

ACTUAL RANGE 2745 N.M. 22° 

(AIR DISTANCE) 

LAUNCH TO FUEL SHUTOFF 

</'-.,,///.r.r/.r~r///,r'/""/J///.r//J/'/..rrE.r/~ 

, , ~ CHECK POiNTS AT ~ , , ~ 50 N, MILES INTERV At ~ ~..r......-.r ... ,../,,,/.rP./,/.r/.//,..//,;/,.r//,,.//.r.///.r> 

Fun OFF~ 

E t::!~c:1_- ~ USNS RANGE TRACKER 

132° 1300 1280 126 0 

proved for Release: 2018/11/16 C0511515 

tAUNCH~ 

- - - PLANNED COURSE 

--ACTUAL COURSE (I!~S DATJ\ FLEXOWRITER READOUT 

ABOARD USNS RANGE TRACKER) 

122" 
TYPICAL MiSSI NS 

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i\\iSSIOt~S ARE DESIGNED BY COMPUTERIZED 

ROUTE PLANNING PROGRAr\'\ 

i3-52H CHINA ROUND TRIP l2000 N. ~,L 

0-218 CHINA MISSION 3000 N. il'l. 

i3-52H RUSSIA ROUND TRIP 9200 N. M. 

D-2JB RUSSIA MISSION 2700 N. M. 

----- -- ------ - - --- - -- - -- - - -- - -

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Approved for Release: 2018/11/16 C05115150 

RECOVERY SEQUENCE 

THE AERIAL RECOVERY SYSTEM EMPLOYED FOR THE D-21B 

HATCH PAYLOAD RETRIEVAL I S A BASIC SYSTEM WHICH HAS 

BEEN IN USE FOR SOME YEARS. THE JC-130B IS EMPLOYED 

AS THE PICKUP AIRCRAFT WITH SEVERAL SUCH AIRCRAFT 

BEING UTlLlLmlN THE OPERATION SO AS TO PROVIDE BACKUP. 

TWO BEACONS AND THE TELEMETRY SYSTEM BRAODCAST FROM 

THE HATCH DURING DESCENT AS AN AID TO THE RECOVERY 

AIRC!I/\FT !NLOCATING THE TARGET. 

THE RECOVERY OPERATION BEGINS WHEN THE Hi\TCH REACHES 

20,000 FEET ALTITUDE AFFORDING THE RECOVERY AI RCRAFT 

SEVEN TO NINE PASSES AT THE TARGET. THIS INSURES A 

HIGH PROBABILlf'( OF AERIAL PICKUP SUCCESS AS DEty10NSTRATED 

DURING THE USAF TRAINING PROGRAM WHEN OUT OF 70 AERIAL 

RECOVERIES ATTEMPTED, 65 WERE SUCCESSFUL. 

RECOVERY ;\1 RCRAFT 

o DiWGUF GU!\! SLUG FI RES 2 SECONDS AFTER 

HATCH EJECflON M·JO DEPLOYS 1)1 LOT CHUTE 

WHi CH DEPLOYS -

o THE DECFlERilTIOr, CHUll '."'HICH flEM,ilINS FOil ]0 

S[CONDS AT WHICH TI!\'\[ IT IS PELEASED AND UPO;\ 

PELEr\ SE I T DEPLOYS 

~ IHE !\If! PICKUP CHUff WHICH IN TLJRi~ DEPLOYSlP THE ~1!\ I N CilU IE \:VI·II Cli Rf MA I ~~ S REEFE D 1'0 Ii 8 

SECONDS \VHEREUf)ON IT 01 SREEFS AND BECOMES 

FULLY INFL/\TED. 

r» i\ B!\ROMETI~! C f~CTUATOR RFLEi\SES ST.II,BI UlATiO" 

r CHUTEilT 20,000 FEET ViHICH AIDS BO/\PDiNG OF 

HMCH BY JC-130B. 

! F A I R RElf< I EV/IL I S NOT rl'l/iDE, HATCH WI L L 

rlOAT AND CAN BE SEA RECOVERED. 

A! R PICKUP CHUTE AT I i~STANT OF ENGAGEMENT 

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