NAS 1.15:100392
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The NASA/Marshall Space Flight Center drop tube user's manual |
1 |
NAS 1.15:100393
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Compendium of fracture mechanics problems |
1 |
NAS 1.15:100394
|
The corrosion protection of 6061-T6 aluminum by a polyurethane-sealed anodized coat |
1 |
NAS 1.15:100395
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Definition of large components assembled on-orbit and robot compatible mechanical joints |
1 |
NAS 1.15:100396
|
Atmospheric environment for space shuttle (STS-34) launch |
1 |
NAS 1.15:100397
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The temperature variation of hydrogen diffusion coefficients in metal alloys |
1 |
NAS 1.15:100398
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Gamma-ray bursts current status of observations and theory / |
1 |
NAS 1.15:100399
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Atmospheric environment for space shuttle (STS-33) launch |
1 |
NAS 1.15:100400
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Atmospheric environment for space shuttle Columbia (STS-32) launch |
1 |
NAS 1.15:100401
|
Estimating the cost of major ongoing cost plus hardware development programs |
1 |
NAS 1.15:100402
|
Equivalent circuit models for AC impedance data analysis |
1 |
NAS 1.15:100403
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Atmospheric environment for space shuttle (STS-36) launch |
1 |
NAS 1.15:100405
|
The charged particle radiation environment for AXAF |
1 |
NAS 1.15:100406
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Concept of a programmable maintenance processor application to multiprocessing systems |
1 |
NAS 1.15:100407
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Preliminary flight assessment of the X-29A advanced technology demonstrator |
1 |
NAS 1.15:100408
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The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane |
1 |
NAS 1.15:100409
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Preliminary flight-determined subsonic lift and drag characteristics of the X-29A forward-swept-wing airplane |
1 |
NAS 1.15:100412
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Preliminary in-flight boundary layer transition measurements on a 45-degree swept wing at Mach numbers between 0.9 and 1.8 |
1 |
NAS 1.15:100413
|
X-29A forward-swept-wing flight research program status |
1 |
NAS 1.15:100414
|
Effect of internal convection and internal radiation on the structural temperatures of space shuttle orbiter |
1 |