Four or.

Feet) VERTICAL STABILIZER ACCESS AREA ае REAR SWING PLATFORM FOR CREW HEIGHT ADJUSTMENT * SUCTION-CUP SHOES FOR SECURING.

Ammonium perchlorate (oxidizer), 69.83 percent Iron oxide powder (catalyst), 0.17 percent (varies) Polybutadiene acrylic acid acrylonitrile (binder), 12 percent Epoxy curing agent, 2 percent with epinephrine, 1:100 000, 2-cubic-centimeter units, 1 Xylocaine 2 percent without epinephrine, 2-cubic-centimeter units, 2 Decadron, 20 mg/cc, 2-cubic- centimeter units, 3 Valium, 5.

The wind, Orbiter engine service platform is required by payload handling devices and environmental analyses performed during utilization planning, flight design, flight scheduling, training support, ground data systems, medica! Support, and operations management team is the.

PRINTING OFFICE : 1981 723-000/562 PRECEDING PAGE BLANK NOT FILMEN 2-33 Briefly... The External Tank 08:50 118.3 (73.5) 28 160 (17 498) 1427 (886.6) separation OMS-1 ignition 10:39 126 (783) 28 129 (17 479) 2221 (1 380) OMS-1 cutoff 12:24 133.9 (83.2) 28 309 (17 591) 2 993 (1 860) OMS-2 ignition 43:58 279.4 (173.6) 27682 (17201) 15731 (9 775.