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GAsTic APOLLO 0 a. xis (cid:9) (cid:9) .../ 0 GUIDANCE 17 (cid:9) ../ (cid:9) -.I (cid:9) VAr‘ (cid:9) Z AND 0 NAVIGATION 2 & (cid:9) 0 (cid:9) SYSTEM 1. MI SD JULY I. 4943 + L SATURN V S-IVB DOUGLAS S-ii SAID ;a( 4 le,- 1 J -2 ENGINE ROCKETDYNE kea,..7104) 75 3 S-IC scr am BOEING 5 J -2 ENGINES ROCKETDYNE P1F, 360 FT 11-4 AP 74372A NORTH AMERICAN AVIATION, INC. SPACE AND INFORMATION SYSTEMS DIVISION ASCENT TRAJECTORY 11501 ALT (FT) 600,000 ORBIT ACQUISITION t 2-- 706 SEC (cid:9) z !!! V-24,280 FPS 5 I 1111 C 7ee (cid:9) - LES JETTISON V.7800 FPS S-IVB IGNITION 300,000 t -.542 SEC 111111111111111h V--= 20,900 FPS S-I1 IGNITION V.7600 FPS 200,000 NITIIII 0L A A A 500 (cid:9) 1000 1500 SATURN V RANGE (N MI) ASCENT PHASE GN-211 (*) EARTH ORBIT POSITION & TRAJECTORY DETERMINATION GN 180 +) - MIDCOURSE POSITION & TRAJECTORY DETERMINATION NEW COMPUTED TRAJECTORY GN-182 (;) LUNAR ORBIT INJECTION START DEBOOST rti c 4_1; 4:4 r c /(,) A 42c; - ic e GN-206A (*) LUNAR ORBIT & LEM DESCENT 1245010439 LEM DESCENT TRAJECTORY CSM HOHMANN TRANSFER ORBIT 80 N MI e 5 CIRCULAR ORBIT r (cid:9) rA4 (cid:9) / (cid:9) inselp. CSM V (cid:127) 5285 FPS (cid:9) LEM INJECTION I-7 I I FINAL AV (cid:127) 98 FPS 1-0--INERTIAL PHASE (cid:9) TOUCHDOWN HOHMANN DESCENT ORBIT PHASE III Z500 SEC (cid:9) - CONSTANT LINE OF 200 N MI N10 N MI LANDING SIGHT SITE PHASE II POWERED DESCENT TRAJECTORY GN-241 LEM ASCENT & LUNAR ORBITAL RENDEZVOUS LUNAR ORBIT (cid:9) ASCENT TRANSFER ORBIT RENDEZVOUS FAM-1006 (M) 64AP76945 LAUNCH AIM POINT DETERMINATION CSM AT LEM INJECTION TERMINAL REND RETURN GEOMETRY ENTRY POINT -INCLINATION GN-204() S/M JETTISON S/M RCS FUNCTIONS -X TRANSLATION 5.5 SEC. + ROLL AFTER 2 SEC C/M ENTRY ATTITUDE SEQ-59B610) ENTRY BOUNDARIES ENTRY POINTS NOMINAL TRAJECTORY PERIGEE OF OVERSHOOT TRAJECTORY ATM OS PHERE INTERFACE VACUUM TRAJECTORY LIP)) GN-205 A ENTRY PROFILE T CX(cid:127) -6.1 ° CM/ SM SEPARATION CONSTA T ATMOSPHERE VACUUM TRAJECTORY 400, 000 FT LAND IN SITE 1500 NM GN-197B-1( ) ENTRY PROFILE = -7.1° GN-197B-24)j OPTICAL OPTICAL r - (cid:9)SIGHTINGS -C INSTRUMENTS INERTIAL OPTICAL GUIDANCE NAVIGATION DISCRETES STEERING ENG NES SIGNALS "ON" a "OFF" GN-9008 SPACECRAFT CONTROL

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MANUAL. DRIVE. CDU BLOCK DIAGRAM. GN-9130. OPTICS . FROM APOLLO . INTERROGATOR PULSE GUIDANCE COMPUTER. L DATA PULSE. +T SET.

Apollo Guidance and Navigation System training slides - Ibiblio PDF

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MANUAL. DRIVE. CDU BLOCK DIAGRAM. GN-9130. OPTICS . FROM APOLLO . INTERROGATOR PULSE GUIDANCE COMPUTER. L DATA PULSE. +T SET.

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Author:	Unknown
Publication Year:	2003
Pages:	56
Language:	English
File Size:	4.75
Format:	PDF
Price:	FREE

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