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Cover image for Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program

Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program

Location Call # Status
Joyner - Microforms B300 NAS 1.15:208472 ✔ Available
Cover image for Launch dynamics of the XM1002 cartridge, 120-mm target practice multipurpose projectile, TPMP-T

Launch dynamics of the XM1002 cartridge, 120-mm target practice multipurpose projectile, TPMP-T

  • 2003
  • Format: Electronic
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Cover image for Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbit

Structural sizing of a 25,000-lb payload, air-breathing launch vehicle for single-state-to-orbit

Location Call # Status
Joyner - Microforms B300 NAS 1.15:210667 ✔ Available
Cover image for Evaluation of thermal sprayed metalic coatings for use on the structures at launch complex 39

Evaluation of thermal sprayed metalic coatings for use on the structures at launch complex 39

Location Call # Status
Joyner - Microforms B300 NAS 1.15:103807 ✔ Available
Cover image for Pre-launch calibration of channels 1 and 2 of the advanced very high resolution radiometer

Pre-launch calibration of channels 1 and 2 of the advanced very high resolution radiometer

Location Call # Status
Joyner - Microforms B300 C 55.13:NESDIS 36 ✔ Available
Cover image for Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware

Simplification of fatigue test requirements for damage tolerance of composite interstage launch vehicle hardware

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Cover image for Preliminary assessment of using gelled and hybrid propellant propulsion for VTOL/SSTO launch systems

Preliminary assessment of using gelled and hybrid propellant propulsion for VTOL/SSTO launch systems

Location Call # Status
Joyner - Microforms B300 NAS 1.15:206306 ✔ Available
Cover image for Deep impact Delta II Launch Vehicle cracked thick film coating on electronic packages technical consultation report

Deep impact Delta II Launch Vehicle cracked thick film coating on electronic packages technical consultation report

  • 2009
  • Format: Electronic
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Cover image for Structural sizing of a 25 000-lb payload, air-breathing launch vehicle for single-state-to-orbit

Structural sizing of a 25 000-lb payload, air-breathing launch vehicle for single-state-to-orbit

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Cover image for A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications

A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications

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