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  • Other Sources  (3)
  • NASA Technical Reports  (3)
  • 1
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    In:  CASI
    Publication Date: 2006-08-29
    Description: Launch operations at Eastern Test Range for Lunar Orbiter 3, 4, and 5 missions
    Keywords: SPACE VEHICLES
    Type: GHT PERFORMANCE OF ATLAS-AGENA LAUNCH VEHICLES IN SUPPORT OF LUNAR ORBITER MISSIONS 3, 4, AND 5 AUG. 1969; P 95-99
    Format: text
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  • 2
    Publication Date: 2019-06-28
    Description: This paper examines the effects of fitting various jet-flap configurations to an AV8-'Harrier II' Baseline aircraft using two NASA developed computer codes. The first code predicts the ground roll of an AV8-B with a partial span jet-flap, a full span jet-flap, a partial span internally blown-flap, and a full span internally blown-flap as well as the Baseline configuration. The second code used was a mission performance estimation routine called ACSYNT (Aircraft Synthesis). This code models each configuration on a standard mission so that the relative merits may be determined.
    Keywords: AIRCRAFT DESIGN, TESTING AND PERFORMANCE
    Type: SAE PAPER 851843
    Format: text
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  • 3
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    In:  CASI
    Publication Date: 2014-02-28
    Description: Prelaunch activities, countdown and launch for Nimbus 3 satellite.
    Keywords: Launch Vehicles and Launch Operations
    Type: THORAD-AGENA PERFORMANCE FOR THE NIMBUS 3 MISSION JUN. 1970; P 63-64
    Format: application/pdf
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