Search wiki using Sphinx

From The Space Library

Jump to: navigation, search

Displaying 1—10 of 14 matches for query "3.15.0.223" retrieved in 0.001 sec with these stats:

  • "3" found 42922 times in 14882 documents
  • "15" found 36664 times in 13784 documents
  • "0" found 2650 times in 1717 documents
  • "223" found 108 times in 103 documents

Above numbers may include documents not listed due to search options.


... 5:20 pm local time (8:20 am EDT) 15 July. The spacecraft entered orbit with a 221.9-km apogee, 186.3-km perigee, 88.5min period, and 51.8° inclination ... -km perigee. The spacecraft was spin-stabilized at 3° per sec with all systems operating normally. Apollo Launch: At 3:50 pm EDT 15 July-7 hr 30 min after the Soyuz launch ... the DM could move ahead. A second maneuver put the CSM in a 223.2-km by 219.0-km orbit. Deorbit began at 4:38 p.m. The command module and ...
... investigators in U.S., Virgin Islands, 15 foreign countries, and ESRO. ''(NASA Release 71-223)'' Results to date of study to determine ... radar system to judge accurate altitude to within two feet (0.6 meters), had shown pilots could land aircraft with greater ... 11 astronauts' emblem-eagle against moon's surface. ''(B Sun, 11/3/71, A6)'' Lack of Government policy for engineering was scored by ...
... as it brightened to a magnitude of 5.3 on the astronomical brightness scale. For approximately 40 seconds ... jet had been composed of a narrow core, 0.4° wide, moving at almost the speed of light. ... Gamma-Ray Burst Was Aimed Squarely at Earth,” news release 08-223, 10 September 2008, http://www.nasa. ... 12 Sep 13 2008 13 Sep 14 2008 14 Sep 15 2008 15 Sep 16 2008 16 Sep 17 2008 17 ...
... Vehicle reached 14 300-m (47 000-ft) altitude and mach 0.70 on flight using two chambers of four-chamber rocket engine ... Earth Resources Technology Satellite Project Team, Goddard Space Flight Center ; OAO 3 Project Team, ARC, Goddard Space Flight Center GSFC , KSC, and ... , 12/15/72, 245; NASA Hist Off; Huntsville Times, 11/9/72)'' National Public Affairs Center for TV began poll of 223 public ...
... Appropriations 15 Aug. plus an amendment to permit NASA to transfer up to 0.5% of its funds between research and development and research and program management programs. The bill appropriated $3.207 ... NASA and community groups and between NASA and state and local governments. ''(NASA Release 74-223; Fletcher memo, 16 Aug 74)'' Dr. James C. Fletcher , NASA Administrator, presented awards at an ...
... Engel, Ludwig, Cand. Ing. Ludwigsburg, Johännesstr. 9 - 223 Engel, Rolf, Dipl. Ing., Montmorency, S. ... 269 Krause, Helmut, Dr., Hamburg-Bergedorf, Vierlandstr. 15 - 79 Krebs, Fritz, Stuttgart-Degerloch, Leinfeldenerstr. ... 81 Lange, Hans-Joachim, stud. ing. Leipzig 0 5, Oststr. 9b - 232 Land, E ... 263 Weirich, Hugo, Dr., Stuttgart W, Silcherstr. 3, II - 115 Weiss, Hans, Augsburg, ...
... 223-lb Cal Tech payload to 146-mi (234.9-km) altitude to study intensity, spectrum, and degree of isotropy of diffuse x-ray background in 0 ... energy spectrum of star X-1 in constellation Scorpius in 0.1- to 15-key range. Rocket and instruments functioned satisfactorily and good data ... space expenditures were averaging about $4.5 billion annually-about 2/3 of 1% of GNP-nearly $4 billion was spent in U. ...
... .). The rocket was to ascend to one km (0.6 mi) at which point the pilot was ... 15 Jahrg., Heft (Issue) 21, 5 November 1933, pp. 365-368; Same article, without a byline, in ''Raketenflug -- Mitteilungen des Raketenflugplatzes Berlin'' (edited by Nebel), Nr. 9, May 1934, pp. 1-3 ... p. 50; Pacific Book Auction Galleries (Seattle, Washington), catalog, ''Sale 223...June 14, 2001, Fine & Rare Books'', n.p. ...
... , THE ORIGIN OF THE MOON'S SURFACE FEATURES, Sky & Telescope, 15-3, 108, Jan. 1956; 15-4, 161, Feb. 1956. 61- R. L. ... AND COMMUNIICATION (U) Rand Rept. RM-1731, 4. June 1956 0 (Confidential) 95 - E. C. Heffern, LUNAR INSTRUMENT CARRIER-VEHICLE DESIGN ... , Sept. 1955 HIGH ALTITUDE ROCKET RESEARCH, Engineering, Vol. 180, p. 223 H. J. Jansen, LIQUID PROPELLANT ROCKET DESIGN CONSIDERATIONS. Aero Digest, ...
... apogee, 755-km (469.1-mi) perigee, 99.9min period, and 74.0° inclination. ''( Goddard Space Flight Center GSFC SSR, 4/30/70; SBD, 4 ... predicted. Space vehicle velocity after boost was 68 m per sec (223 fps) lower than planned, causing S-IVB orbital insertion burn to ... extra clothing. April 15-17: MCC-5 at 145:19 GET, by 15-sec Lunar Module LM DPS burn, decreased velocity by 2.3 m per sec ...

Additional database time was 0.095 sec.


Result page: 1  2 
 
Search in namespaces:

















Powered by Sphinx
Views