"The
plaintiff’s wish to correct what he regards as a widespread misconception about
those who served the nation under the Articles of Confederation is laudable."
--
Steven
D. Merryday, United States District Judge
Evaluate effects of prolonged space flight. Demonstrate and evaluate
performance of spacecraft and systems in 4-day flight. Evaluate
procedures for crew rest and work cycles, eating schedules, and
realtime flight planning. Spacecraft weight: 3574kg.
Secondary objectives included: Demonstrate and evaluate EVA and
control by use of HHMU and tether. Stationkeep and rendezvous with
second stage of GLV. Evaluate spacecraft systems. Make in-and-out-of
plane maneuvers. Further test OAMS retro backup capability. Perform 11
experiments.
Launch:
June 3, 1965 10:15:59.562 am.
Orbit:
Altitude: 296.1 km (159.9nm)
Inclination: 32.5 degrees
Orbits: 62
Duration: 4 Days, 1 hour, 56 min, 12 seconds
Distance: km
Landing:
June 7, 1965. Landing was at 27deg 44min North and 74deg 11min West.
Landing was 81.4km from attempted landing zone.
Mission Highlights:
Gemini-4
was NASA's 1st Extra Vehicular Activity (EVA) operation. EVA time
36min
All but one primary objectives were achieved. Computer controlled
reentry in the demonstration and evaluation of spacecraft systems
objective was not flown because of inadvertent alteration of computer
memory. All secondary objectives were met except one. The secondary
objective of stationkeeping and rendezvous was only partially
successful because separation and rendezvous was not attempted due to
fuel consumption.
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For ORDER:"The
plaintiff’s wish to correct what he regards as a widespread misconception about
those who served the nation under the Articles of Confederation is laudable."
--
Steven
D. Merryday, United States District Judge
Keynote Address on the 2003
Re-Internment of Samuel and Martha Huntington
Cyrus Griffin
10th President of the United States
in Congress Assembled
January 22, 1788 to January 21, 1789
Keynote Address on the 2003
Re-Internment of Samuel and Martha Huntington Part II
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