Apollo 204 Review Board Appendix D - NASA's History Office

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° -_ . o. - . .. _.. o o. _:" "- : APOLLO SPACECRAFT The SpVvL ._i_" "'. "'O_.sists of a launch escape system(LES) assembly, co_ .-" _ • . , ..C/_, '). .,, ser,,'ice module (S.;M), and the spacecraft/ lunar module adapter (S|.AL 1he [.ES assembly provides she r,_eans for rap,dl'_ .,.epa_a;m_ the C M t_om the S.'M d_rm_ p_d or subolbital aborts. "l'he C/M iorms the :spacecraft control center, contains necessary auto- marie and r0:,nual eqmpmenl 1o control and treonitor the spacecraft s v'.:tem'._, and contains the reqtiired equipmen: for safety and comfort of the ere,,..', lhe S/3| is a cvlindrical s.ru,-,ure l_ated between the C/M and th-'_- SI.A. I_ contain.,, the ptopul'_ion :-,vslems for attit_.¢le and veloc- ity chan,4e maneuvers. Mo_,t of thc .nsurnabi=_; used in the missicrn are stored i, the S,'M. The SLA is a Irup, caled cone which ccnnects the S.'M to launch vehicle. It al,-o prm_des the space wherein the lunar 171_]U!V -'_ri-led oll h:Flai I}11_,,,1 lq_° .. TS_",_,y It, l PROGkES$ AT TIfF OF ACCIDENT Spacccra,':_('.: "a:;der_r:ing a "Plu_ O,Jl Int,'grated "Fes_" at ti-_e lime of II, ,L .'_...* o_1 January 27. 19_i7. Operational Checkout Proce- dure, aesir, _ " _.,.CP FO-K-00'21-1 applied _o 'his test. Y-'ithin this r,.port this procedure _s often referred to as OCP-0021. I"ESTS AND ANAt.YSF$ Results of tests and analyses not complete at the time ofw_blication of this report will be contained in <strong>Appendix</strong> G. Addenda and Corrigenda. CONV.E_.$10.q OF TI,_'[_ "l'hrou'.no'al tbi'_ r..po:t. _:m _'. ";_a_cd _, (;r:c ',"_c_" _/can "Ii_: (GLFF). To convert f;MT to Easterr_ Standard Time (I--S'I). subtract 17 hours. For ex:m_p',e, 23:31 G?',"F c:_._;'_'r!c'd _ 6:_1 p.:':, r:.ST. © ©
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Apollo 204 Review Board Appendix D - NASA's History Office

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