NAS 1.60:2019-220321
|
Target optimal aperture selection |
1 |
NAS 1.60:2019-220343
|
Suited ground vacuum chamber testing decompression sickness Tiger Team report |
1 |
NAS 1.60:2019-220391
|
NASA lunar lander reference design |
1 |
NAS 1.60:2019-220401
|
Effects of the Serber first step 3DHZETRN-v2.1 |
1 |
NAS 1.60:2019-220419
|
The Badhwar-O'Neill 2020 model |
1 |
NAS 1.60:2019-220552
|
Calculated transmission using a portable spectroreflectometer |
1 |
NAS 1.60:2020-220185
|
Stochastic simulation of mudcrack damage formation in an environmental barrier coating |
1 |
NAS 1.60:2020-220443
|
An adverse outcome pathway for potential space radiation induced neurological diseases |
1 |
NAS 1.60:2020-220514
|
Simulated galactic cosmic ray and solar particle event radiation effects on inflatable habitat, composite habitat, space suit and space hatch cover materials |
1 |
NAS 1.60:2020-220584
|
Evaluation of fatigue damage accumulation functions for delamination initiation and propagation |
1 |
NAS 1.60:2020-5001740
|
Double-differential FRaGmentation (DDFRG) models for proton and light ion production in high energy nuclear collisions valid for both small and large angles |
1 |
NAS 1.60:2020-5005040
|
Electron beam freeform fabrication of dissimilar materials : cracking in Inconel® 625 deposited on GRCop-84 |
1 |
NAS 1.60:2020-5007062
|
Hardness-strength correlations in Zr(Cu)-based BMG alloys for QA purposes |
1 |
NAS 1.60:2020-5007433
|
Urban air mobility noise : current practice, gaps, and recommendations |
1 |
NAS 1.60:2026
|
Establishment of a rotor model basis |
1 |
NAS 1.60:2032
|
Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder |
1 |
NAS 1.60:2074
|
Flightweight radiantly and actively cooled panel : thermal and structural performance |
1 |
NAS 1.60:2184
|
Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept |
2 |
NAS 1.60:2284
|
Space shuttle orbiter trimmed center-of-gravity extension study : summary report |
1 |
NAS 1.60:2345
|
Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes |
1 |