34704fe73bfeb1a9

40989256-001

NARA·NARA_AirIntel_17618564·tiff_group··80 pages

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LR RUNS ETD AAEM SRNL ER TEL RSE CE, PROP ETE A MF RAORELTT CASTLES, BEET IRENE RL ADEE AE STONER STEELE TE a CSR RST TELE A RAE ES ERLE TC AO : FLIGHT FOLDER CHECKLIST he Bas OET LCA CHECK CHECK I. FLIGHT FOLDER CHECK LIST: (AFCRL FORM 25) A. FLIGHT REQUIREMENTS DOCUMENT (AFCRL FORM 24 OR 24A) 8. SCHEDULE REQUEST (STEWS NR FORM 1) C. SCIENTIFIC BALLOON USER DOCUMENT (AFCRL FORM 104) Il, PRE-LAUNCH AND LAUNCH INFORMATION A. PRE-FLIGHT BRIEFING (AFCRL FORM 99) CREW CHIEF REPORT (AFCRL FORM 22) HELIUM INFLATION COMPUTATION SHEET (AFCRL FORM 21) BALLOON LAUNCH/LAYOUT DIAGRAM FAA BALLOON FLIGHT NO
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cou AIR FORCE BASE, NEW MEXICO 88350 1. The following personnel ‘are assigned to support a scheduled balloon launch at 0600 hours, IL Apri Z8 3 Personnel will report on dates and times indicated. A pre- flight briefing will be conducted in the Conference Room at 1745 hours 7 7 April 78 Project Officer Mr. Ground _ Launch Officer /NCO = =. NAS. Test Coordinator _ oo Scientific Investigator NAS LAUNCH CREW (REPORT __0300_ Crew Chief _—-Mr. Fumerola West Crew Chie. oy ie Launch Vehicle Driver Mr._ Wofford — es Mer stauber Mr. Butko ee ae UMr. _ Bean Instrumentation : “Mr. Cordery _ "Mr. Mares CON
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RECOVERY: STILE. VOLUME (S) orl Oe 10° LTV Uz : _|SUBBLE TO BE scts| CUT OFF LO @) DO NOT AC OPS RASC DONTE NAY PARA NRSC WO ASE SUNS aA TNL: cnet GROSS IGH 1130 DROPPABL i b SA EU CRN OI EESTI MRA SCORE SESE 3. RADIOSONDE Laping Mod STANDARD —. COMMA NOS: 4, Beacon off (Antenna dr P).@ Valve F: on On (Latch) _ts) Sampler On_, qs) Pour Ball (6) Sampler Off (9)_ Terminate x ween NON-SEQUENCED : (3) Ballast ST (Type, Container, Total Flo So ee satin Sa ei = is Glass/ De oppers/3 eee Class77 | SUE SOSH Si ene ee eer SEPARATION DEVICE ———— DIAMETER (S) Qual Cannon Cutters 4 iMPACT SWITCHES x ee} E
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DFS (TY 1) a (DOE) use ) c ec. Single 12V pack BB-405 Auxiliary COMA LT RLS pack - Backup 12V_pack 6HE - Balloon strobe TRE TTA gle 15V pack ar — g. Single 12V pack 1 imary instrumentation 1 | | ig period ntrolled program IAW SCADS-2 check list. | | 6 f i ide Sensors -60 (densimeter) TLM Ch #1 a Rosemount 3B gondola will be flown with two 10K nylon stra er ——— ScD RS ESE ELE SLED WORE AS LET, SPEER LE TE TE cs mune Ss ASN ELE EL TOTES IA VIRGEN 2 ER
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> Composition buNCH/INTERCERT/DwAcT/ 11 Seo- SENENT SO | © ;  pvent. source. OG00s ie beuieh = 20 ieee Rnwy O4 P-A/C 1200 _1300 Roswell, NM C-130 Practice | PATTERN = Aerial Catch Co: ceca (OLS) Agere perk P-138.06 MHz P-9019.5 KHz Pp-hO.35 P-1746 practice aerial catc SURVEILLANCE RADAR | _ 7: | 2 \3 if 4 5 STEWS -NR-R SOP 70-4H
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a BRIEFING DATE/TIME Toahpr (8/1 1300 MST FU H ER _H78-13/H-129 “Yo. PROJECT OFFICER 2 RslCary ee ea cud 4, FLIGHT OBJECTIVES: A, Collect T Two. DFS” Te Lversa for, DOE_ B. Collect cS Li Sample for DOE c, ' D FL GH f FEL s = 6. “TEST COORDINATOR i > N BULED LAUNCH: A. SITE Holloman AFB, NM. | Fumerola a0 B. pate/time 11 Apr 78/0600 MST | | | | ES ST ST RE RR 40. TE RMINATION DATE/TIME ee Le: AYLOAD 11 Apr 78/1200 MST _ 800 lbs me 3 AL LOON NO. “MANUFACT URER Winzen LENGTH(S) 5. VOLUME (5) 3 i i 6 150. he ah Se eee! foe so Wiel ea Ome . iM RIEL & THICKNESS 330, dbs C7 raat in ea VALVE & : VALVE
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OPPABLE BALLAST i) N SAFETY TIMER: MINUTE BE KFT ve yg) 3. TERMINATION TIMERS: A. PRIMARY B. SECONDARY 9 hrs > IMPACT SWITCHES A. ARM ALTITUDE i ithe uation eal lial iS RADAR REEUECTORS Semis oe ~ [16. FLASHING LIGHT LOCATIONS _Not Required Package & BEF Aamo noemaerenienenenn A NACA RE HR RN GRO er OC RA NE NG CMR SR AN SERENE PORES SF DERE UNICA ATIONS DATA RSPR nr 9S EAD HE IER ATR REN ANION Pst PRA NC AENEAN OTR OA ANNO EON OO a ee A HeO) WOT 742 5708 13) BOB an VHEU eG 2 bi 5s ae uHF() = N/A (2) N/A D. SPECIAL N/A CALL SIGNS: As CONTROL CENTER Fishhead Control B. VAN N/A Srecoveay: N/A ee
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eS EW CHIEF REPORT a eee 13 April 1978 PROJECT NO. _Ash Can BALLOON FLIGHT NO, BALLOON NO. H78-13/H-129 S208 ITEM ie CONTRACT NO. 4 002 F29651-77-90051 MANUFACTURER SERIAL NUMBER Winzen 26 BALLOON DIA 108.08 ft VOLUME TAPES (No. & Type) .516 MCF 54 Tailored MATERIAL & THICKNESS Stratofilm/1.5 mil BALLOON LENGTH 55 HOett NO. INFLATION TUBES NO. OUCTS al 2 TORQUE VALUES TOP 44" lbs BOTTOM N/A: RELEASE VEHICLE Crane | LAUNCH PLATFORM © 119L iTEM __WEIGHT/LBS __1TEM WEIGHT/LBS VALVE TYPE & WEIGHT EV-13 Sic 9.0 BALLAST BALLOON LAUNCH Glass Ballast 337.0 BALLOON MAIN Nitrogen Gas_ SEPARATION Device 

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