Showing posts with label testing. Show all posts
Showing posts with label testing. Show all posts

Saturday, January 24, 2015

Space1 Ground Safety


SPACE1 GROUND SAFETY
Space1 is all about safe space, safety, and making space travel safe for human astronauts and space tourism. Space1 has also focused efforts on making down-to-Earth safe space.

— space safety is no accident⠀—

SUMMARY
Safe space is on everyone's mind from the beginning of the space program in the 1950s. However, it takes new innovation to bring dreams into reality.

People want safe space travel. Fewer people consider ground safety. Work continues at Space1 using a method of ground testing safety assurance. The new GTSA methods assure a good safety record for materials handling and storage, rocket and engine testing, and management of the launch and related factors such as weather dynamics.

ISSF Space safety magazine
METHODS
Safety adds up whether on the ground or in the air. The latest addition to our flight safety management program FSMP is a special safety observatory that can observe, monitor, and assess the atmospheric "seeing cell" in the determination of ground and flight conditions.

Creating and maintaining safety requires an important understanding of varied conditions and a balance of factors.

FACTORS TO CONSIDER
pressure, temperature, humidity, turbulence, strata, solar, rain, cloud, sinking or rising air, wind, ice, sleet, snow, hail, trade winds, jet stream, down-drafting, up-winding, rider cells, shade, zonal stratification, evaporation, dew point, season, radiation, shearing, weather indices, moisture variance, ramping, cooling, heating, expansion, contraction, impending gradients, retentive condition, elevation, differential mode, circulation, convection, hydrological cycle, atmosphere-biosphere interactions, rivers, lakes, oceans, land masses, elevated obstacles, biogeochemistry, low high density, ice-ocean coupling, heat exchanges, soil interactions, ice sheeting, aerosols, day/night morning/evening conditions, tidal conditions, planetary conditions, Coriolis effect, molecular carbon trapping, effects from cyclones, tornadoes, hurricanes, typhoons, distant storms, electrical discharge, static conditions, gusts, flanking drafts, lenticular anvils, lithosphere conditioning, cryospheric emination, tropospheric delineation, spill overshooting, and various conditions with anomaly and other predictive states.

Friday, December 26, 2014

Multi-D Invention for Space1

The Multi-D invention can undergo development and testing in the Multi-D Laboratories controlled environment chamber. The Lab has a level safety net for level I testing. Level II must be isolated outdoors for safety reasons.
THE MULTI-D INVENTION FOR SPACE1
 
INTRO
Humanoido has invented the spectacular and powerful Multi-D invention for Space1. The Multi-D Imaging and Testing Lab is now established for testing and development of this remarkable device.

OPERATION
In the actual machine, the Multi-D can have flight in various positions relative to the tourism rocket's flight during the flight mission. With its mind remotely controlled, it can move to anywhere in the dimensional matrix grid and then datalize. So essentially there are two changing vectored flights.

SYSTEM CALCULUS

This is defined by the dual calculus of the differential equation of changing orientation of two flight paths. It can provide spectacular sci data and views, ideal for many purposes of the space tour, of data for space flight, of show for investors and for tourists. It will become an integral part of the space tourist system.

NASA DREAMS
NASA wanted something like this for Space Shuttle missions, but it never developed it. If NASA had developed it, it could have helped recognize the anomalies that led to the crash of Space Shuttle Columbia on Feb. 1, 2003.

SPACE SAFETY
Safety is paramount in Space1's Tourist System, which includes the Safety Rocket invention. Multi-D may seem like a safety redundant system feature, but its many additional uses are remarkable.

DEFINITION
Multi-D stands for Multi Dimensional, and refers to the ability for the system to move within a multidimensional grid or matrix framework relative to a changing source, in this case the tourism rocket.

EXTRAPOLATION
Extrapolating some ideas of Multi-D, it could serve as a time and space calibration for the RTM Referential Time Machine. It could also have telemetric interfacing to the avataric connection in real time, though the complexity of this may require additional design work.

Monday, January 3, 2011

Testing Setup for LEDs

01-03-2011, 05:00 PM Code 6-102 TESTING SETUP FOR LEDS

Testing setup for LEDs using breadboards mounted on Parallax Propeller Proto Boards.

Testing Conclusions

01-03-2011, 01:55 PM Code 5-98 TESTING CONCLUSIONS

    * The decision is made to use on-PPPBs data lights with 4K7 resistors.
    * The on board data light will be kept for more infrequent use
    * Modified boards will be used throughout the Brain Stem, Brain Base and Brain Span
    * A red LED will be selected over green and yellow

Power Testing

01-03-2011, 01:55 PM 5-97 POWER TESTING

    * Modified Parallax Propeller Proto board (both regulators and LED disabled) draws 4mA idle. Power LED converted to data light draws 20mA when on. Another test confirmed 4mA modified board current. Unmodified, board draws 10mA. To modify, lift the middle leg of the 3.3 vdc (output leg) of the LM1086 CS-3.3 regulator.

    * Another test, mod proto board draws 5ma, 19ma with on board data light. Put Taiwan LED on pin 25 with 150 ohm resistor = 12ma. Draws 6ma with 2.2k ohm. (since board draws 5ma, the Taiwan LED is drawing only 1ma)

    * Power LED converted to data light still has a 241 ohm resistor on it which is too small a value and that is why you see 20ma current. This is not acceptable for the purpose of battery portable operations. Therefore another data LED will be added.

    * The China red LED is the same as the red Taiwan LED – very bright at only 1ma. The green China LED is barely visible. (using a 2.2K ohm resistor). The green Taiwan is also too dim. The yellow Taiwan LED is also the same/ too dim.

    * The secondary LED was tested with a 2.2K resistor and was bright. With a 4.7K, it was less bright but still usable. You would not want to go dimmer. Therefore, with the Prop's 3.3 volt pin, use a resistor from 2.2K to 4.7K range depending on desired brightness. Both tests showed the LED drawing 1ma.