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... , Va. Initial orbital data: 843-mi. apogee, 180-mi. perigee, 101-min. period, and 52° inclination to the equator. Under overall administrative responsibility of the British Office of the Minister for ... . (147-mi.) apogee; 192-km. (119-mi.) perigee; 88.7-min. period; and 64.8° inclination to the equator. Soviet news agency Tass said the satellite carried scientific instrumentation intended for ...

... data: apogee, 395 km. (245 mi.) ; perigee, 209 km. (130 mi.); period, 9038 min.; and inclination, 65° to the equator. Scientific equipment onboard the satellite was "intended for the further exploration ... time the probe was in the following position: right ascension, 5 hrs. and 56 min.; inclination, minus 4° 22 min. Experimentation With ZOND I continued. ''(Tass, Krasnaya Zvezda, 4/5/64 ...

... maneuvers in the area of the equator, the space vehicle substantially changed the angle of inclination of its orbital plane." After the programmed space maneuvers, POLET II was in the following ... : apogee, 500 km. (311 mi.); perigee, 310 km. (193 mi.); period, 92.4 min.; and inclination to the equator, 58.06 degrees. ''(Tass; Shabad, NYT, 4/13/64, 4)'' Gemini spacecraft ...

... ''(222-km)'' apogee, 101-mi ''(163-km)'' perigee, 88.3-min period, and 31.63° inclination; nose cone jettisoned; space­craft coasted for 43 min 52 sec; and LM separated from ... ''(222-km)'' apogee, 104-mi ''(167-km)'' perigee, 88.4-min period, and 31.63° inclination. Initial 39-sec DES burn, designed to simulate deceleration for descent to lunar surface, was ...

... -km)'' apogee, 112-mi ''(180.2-km)'' perigee, 90.6-min period, and 81.5° inclination and reen­tered Feb 27. Other satellite entered orbit with 338-mi ''(543.9-km)'' apo­gee, 294-mi ''(473.1-km)'' perigee, 94.9-min period, and 81.7° inclination. Flights were fifth and sixth since LTTAT vehicle was activated on May 9, 1967. ''(SBD ...

... -mi)'' apogee, 211-km ''(131.1-mi)'' perigee, 91.2-min period, and 48.4° inclination and reentered March 24. Cosmos CCIII entered orbit with 1,203-km ''(747.5-mi)'' apogee, 1,186-km ''(736.9-mi)'' perigee, 109.2-min period, and 74° inclination. Both satel­lites performed satisfactorily. ''(UPI, P Inq, 2/21/68; SBD, 2/21/68 ...

... -km)'' apogee, 346-mi ''(556.7-km)'' perigee, 199.5-min period, and 100.5° inclination to determine flexibility of cadmium sul­fide solar cells in space and to measure proton ... -km)'' apogee, 348-mi ''(560.0-km)'' perigee, 207.8-min period, and 100.0° inclination. ''(UPI, C Trib, 4/8/68; SBD, 4/9/68, 220; GSFC SSR, 4/15 ...

... -mi)'' apogee, 248-km ''(154.1-mi)'' perigee, 92.1-min period, and 48.4° inclination. Instruments functioned nor­mally and satellite reentered Nov. 2. ''(SBD, 6/13/68, 215; GSFC ... Dandridge M. Cole Memorial Lecture before AIAA Greater Philadelphia Section: Poll after poll showed "strong inclination to slow down or cut back R&D-particularly the space program. . . . Indeed, sentiment has ...

... ''(5,884-km)'' apogee, 397.7-mi ''(640-km )''perigee, 157-min period, and 59A° inclination. Apogee motor was fired July 7, placing Explorer XXXVIII into planned near-circular orbit with ... , 3,641.2-mi ''(5,860-km)'' perigee, 224.4-min period, and 59.2° inclination. On July 8, yo-yo despin mechanism reduced spin rate from 93 rpm to 2 ...

... -km)'' apogee, 94-mi ''(151.3-km)'' perigee, 103.0-min period, and 89.8° inclination and reentered Nov. 6. OV 1-16, nicknamed "Cannonball," was 600-1b, 23-in-dia ... mi ''(460.3 km)'' ; perigee, 82 mi ''(132.0 km)'' ; period, 90.4 min; and inclination, 89.8°. OV 1-16 reentered Aug. 19. ''(O'Toole, W Post, 7/12/68 ...

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