UAH Archives, Special Collections, and Digital Initiatives

Browse Items (8023 total)

  • iusivbforskiorbandtratheana_081707134156.pdf

    This report determines the maximum and minimum solar and terrestrial thermal energy incident and absorbed by Saturn IB/V vehicles in earth orbit and translunar travel. The influence' of this external energy on the Instrument Unit Thermal Conditioning System performance, and consequently its adequacy to maintain the electronic packages at acceptable temperature limits is ascertained. Conclusions are: a) Methanol/water coolant temperature will deviate from 111 specifications only during translunar cold flights. However, adequate thermal conditioning of the electronic equipment would still be maintained. b) Instrument Unit missions exceeding 6 1/2 hours, or electronic packages heat dissipation magnitudes lower than 3 kw or higher than 8.5 kw, should be reviewed to ascertain thermal compatibility.
  • http://dkdayton.net/roberts/images/r10/pdfs/r10_02-20.pdf
  • Johnfkennspaccent_120408110048.pdf

    This is primarily the bibliography of an organization located in an area which was once inhabited by more beasts and birds than people. The evolution of the Kennedy Space Center cea be traced from the Army Ballistic Missile Agency and Marshall Space Flight Center, Huntsville, Alabama. That period is fully covered by Historical Origins of NASA's Launch Operations Center to July 1, 1962.
  • Johnkennspaccent_092507162139.pdf

    This is primarily the bibliography of an organization located in an area which was once inhabited by more baasts and birds than people. The evolution of the Kennedy Space Center :LS :A .ceable from the Army Ballistic Missile Agency and Marshall Space Flight Center, Huntsville, Alabama. That period is fully covered by Historical Origins of NRSB's Launch epesons Center to July 1, 1962. However, because of the core working relationship between the Kennedy Space Center and the Air Force Eastern Test Range articies showing evolution of the Air Force Missile Test Center are included.
  • sdsp_skyl_000067_001.pdf

    This is a report about the Skylab 1 reentry.
  • Skywriterjun1369_121410150031.pdf

    News article covering NASA's announcement of Apollo 11's launch-date: July 16th.
  • Skywriterjun669_121410150523.pdf

    News article confirming NASA's announcement of Apollo 11's launch-day. Focuses on the optimism surrounding the launch as well.
  • spc_spac_000359_000360.pdf

    This flier has a colored image of the "Junior Hot Rod Ride" as well as a description and price for it.
  • JunoVspacvehi.pdf

    The initial phase of the JUNO V space vehicle development program, as presented herein, provides for a static demonstration and a total of four flight feasibility tests. The latter two flights will give the U.S. its first payload capability in excess of 10,000 lb in mid 1961. The objective of the overall program is to provide a reliable, economical, and flexible carrier vehicle with relatively large payload capability for orbital and space missions at the earliest possible date.
  • junovvehiclers_022107152001.pdf

    This report io the second in a scrics of reports on the JUNO V Space I Vehicle Development Program and indicates the present status of the overall I program. The objective of the overall program is to provide a reliable, economical, and flexible carrier vehicle with relatively large payload capability for orbital and space missions at the earliest possible date.