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LOST LESSONS

 

HARDWARE DEVELOPMENT FOR

TEACHER IN SPACE ACTIVITIES FLIGHT 51-L

By Bob Mayfield

Hardware design and development began at Johnson Space Center in August 1985.  Although a number of people contributed to the proceeds, a talented team of engineers from Pan American Engineering and the personnel in the shops at Johnson Space Center comprised the backbone of the process.

The Teacher in Space Project (TISP) involves six activities which will be filmed and photographed during the mission and two live lessons aired on flight day 6.  The six activities are listed below in the order in which they will be conducted.  A discussion of some of the rationale for the hardware design follows: [The following are henceforth identified as the lost six.]

HYDROPONICS

MAGNETISM

NEWTON’S LAWS

EFFERVESCENCE

CHROMATOGRAPHY

SIMPLE MACHINES

Before discussing each activity, it is probably appropriate to relate  some of the general constraints that applied to the payload in general.  First, it had to fit within the confines of one mid-deck  locker (approximately 17"x14"x22").  It had to pass off-gas tolerance criteria.  This eliminated or restricted the use of many plastics, metals, adhesives, and liquids.  Obviously, it had to be safe and not interfere with the operations of the Orbiter's systems.  Also considered was the flammability of the materials independently and collectively.                                                                                             

Other constraints were established by the perceived goals of the project.  For instance, it was important that teachers in the classroom would be able to closely duplicate the equipment and conduct demonstrations to be used as a comparison of the behavior of phenomena on Earth and on-orbit.  It was believed that highly exotic hardware would inhibit the involvement of some teachers and student groups. The range of age levels had to be considered.  The action, interaction, or reaction of components had to be clear in order to be filmed and photographed.                                         

Finally, the number and variety of the activities, plus the equipment to support the live lessons precluded the possibility for the education staff to develop viable quantitative science experiments of each activity in the time allotted to produce the hardware.  Therefore, the activities had to be considered qualitative demonstrations.

HYDROPONICS

 

Click on link below to go directly to the Lesson Plan:

 

HYDROPONICS LESSON PLAN

The goal of the hydroponics activity was to demonstrate a possible procedure that might be used on the Space Station and in future space endeavors to provide nutrient requirements in a closed environment in microgravity.  The objective was to demonstrate the processes related to growing plants in microgravity.       

The lesson plan called for two white beans to be germinated per day beginning 7 days prior to launching.  One plant from each pair would have been selected for flight, contained in its own closed hydroponics system.

Several problems emerged.  White beans take several days to germinate.  They produce large plants quickly after emerging.  The absence of good light for plant growth on the Orbiter would have aggravated the latter problem by causing the plant to be "leggy" or elongated. There would not be room in the locker to accommodate adequate containers.  Mung beans had better characteristics and had been flown on a previous mission, providing some baseline information.  The number of plants was reduced to six due to payload volume constraints, and it was decided to use three seedlings 2 days old and three newly germinating seeds to reduce the overall time involvement by ground support staff with this single activity.

Hydroponics in Space Lesson

Aboard the Zero-G Aircraft, Christa Applies Misting to Chamber 6 which will hold a  Mung Bean  

Another major problem was that of providing a substrate for the plants that would allow for growth while keeping the fertilizer fluid where it belonged.  A number of ideas were tested with the help of volunteers such as Cheryl Barnard, an undergraduate student at the University of Houston , and John St. John, an eighth grade student from Friendswood , Texas ,  The final design consists of a 1/2-inch layer of polyester fiber sandwiched between two lexan rings.  Nylon mesh was glued to the upper side of the bottom ring to hold the fiber.  The rings are separated by two stainless steel tubes 1/2-inch long.  Two screws fit through the tubes to hold the platform together.  Two longer screws secure the platform to the top of the 2-inch diameter cylinder.  The seed is nestled into the fiber.  This configuration was accepted for its relatively simple design, keeping in mind the fact that to be cost effective on a large scale, such as in the Space Station, the simplest workable system would be desirable.                                   

Hydroponics Chamber

Another aspect of this activity is the root misting apparatus in cylinder number six.  This idea was stimulated by experiments at the Epcot Center .  The roots of the plant in this cylinder will be misted once a day.  If this plant remains as healthy as the others, perhaps such a weight saving system could be employed on a large scale in the Space Station.


Close View of Hydroponics Experiment Apparatus

MAGNETISM

 

Click on link below to go directly to the Lesson Plan:

 

MAGNETISM LESSON PLAN

The goal of the magnetism activity was to understand the role of magnetic lines of force in the space environment.  The objectives were to photograph and observe demonstrations of magnetism in space, and to photograph and observe lines of magnetic force in three dimensions in a microgravity environment.           

A compass and bar magnet readily procured from a teacher supply store were selected to demonstrate that magnetism certainly is a force in microgravity.  The magnet had to be stripped of its plating material and nickel plated to make it pass off-gas criteria.


A box made of aluminum or some other nonferrous material, holding iron filings, and covered by a transparent top was proposed as a means of demonstrating lines of magnetic force in two dimensions.  It soon became clear that a sandwich of two lexan plates separated by a "gasket" of lexan would occupy less volume and be easier to fabricate.  Two tiny holes were drilled in one plate to preclude problems of pressure differential in case of a contingency EVA causing the cabin pressure to be lowered.  Safety considerations precluded the use of iron filings which might have been ingested by crewmembers or electronic equipment if accidentally released into the cabin.  Instead, soft iron wire (baling wire) was cut into lengths 1/8- to 1/4-inch long for use in this and the other magnetism demonstration.  These wire pieces had to be coated with nickel oxide, soaked in oil, then baked to prevent rusting.  They were also tumbled with ball bearings 24 hours to remove sharp edges.  Some tests were done using #6 steel shot, but thelinear wire pieces gave the best results.       

The original proposal for demonstrating lines of force in 3-D called for a transparent beach ball with an electromagnet suspended inside. An exhaustive search for a suitable ball was futile.  Therefore, a cube was constructed of the same material found covering the drink containers used on the Shuttle.  Tests proved its optical qualities were acceptable, it was tough, and could be bonded using equipment at the Johnson Space Center .  It was believed that the cubic shape would cause the least problems with reflections during filming.       

The electromagnet evolved out of much testing of suitable core materials, wire sizes and lengths, and battery configurations.  The final product consists of 400 feet of copper magnet wire around a 3-1/2 inch soft iron bolt 1/4-inch in diameter.  The resulting magnet is 3/4 inches in diameter.  Soft iron does not retain magnetism when the power is turned off.  Power is supplied by two "AA" batteries wired to a toggle switch with built-in LED, and a variable resistor with a range of 0-250 ohms.

 

 

Magnetism Lines of Force in Space Lesson

 

 

 

Though this electromagnet is not strong enough to hold the wire pieces in 1 g, tests on the KC-135 weightless trainer proved its effectiveness in microgravity conditions.  A more powerful magnet was not used to preclude interference with the Orbiter  systems.      

 

An additional problem to be addressed was the introduction of moisture from the breath as the cube was inflated.  The resulting condensation obscured viewing into the bag and caused rusting on the approximately 4000 wire pieces inside.  Solving the problem included treating the wire as previously described and putting a desiccant filter in the inflation tube.

 

NEWTON’S LAWS

 

Click on link below to go directly to the Lesson Plan:

 

NEWTON'S LAWS LESSON PLAN

 

The goal of this activity was to demonstrate the fundamental laws of motion during weightlessness.  The objectives were to show the principle of inertia in an orbiting spacecraft; to show the relationship between force, mass, and acceleration; and to show the action-reaction of two different masses colliding.                                    

To first demonstrate that objects have no apparent weight .in the spacecraft was relatively straightforward; an object would be suspended in midair on a small spring.  The spring would not stretch because the object is in free-fall around the Earth traveling at the same rate as the spacecraft.  If the end of the spring were attached to the inside of the craft and a thruster were fired, it would cause the spring to stretch due to the spacecraft changing velocity with respect to the object.            

Determining how to demonstrate the objectives was not so straight-forward.  Historically, educators have disagreed on methodology for treating this topic.                 

Add the educated opinion of engineers and technically oriented support staff to the realities of the Orbiter environment and the problem became very complex.            

There was discussion of using objects such as wooden blocks of different sizes, therefore different mass; except some of the activity called for objects of the same size, yet 1/2 or 1/4 of the mass of each other.  This would have meant finding materials whose densities varied with the desired proportions, or mechanically altering (drilling holes) in one of the objects to achieve the desired effect.  The wooden block idea sounded plausible until flammability and off-gassing were considered.  Using metal blocks was considered and dismissed, remembering the criteria of keeping the hardware within the ability of teachers and students to copy as closely as possible.  Overall payload weight (pre-launch) was also considered - metal masses large enough to be filmed effectively would have been relatively heavy, even using aluminum.  Another problem with blocks would have presented itself when the teacher attempted to use whatever triggering device was developed to exert a force on the object.  If the forces were not exerted precisely through the center of mass of the block, it would tumble and not move as desired.  A sphere would not present this problem.      


The decision to use spheres created a new challenge: making spheres of common substances acceptable for flight in a manner available to the public.  The challenge was met by acquiring a billiard ball, then locating a steel ball bearing whose mass was almost exactly 1/2 its mass.  Conveniently, the diameter ratio of the spheres was almost exactly 1 to 2 also.  The ball bearing used was 1-1/8 inches in diameter.                                                                                                                  

Another problem to address was the force actuator or trigger device.  Some means had to be provided for the teacher to apply the same amount of force to different objects accurately, repeatedly, without imparting other influences.                  

Using the retraction mechanism of a ball point pen was considered.  This posed difficulties.  Though the teacher would be able to exert the force through the center of mass of the sphere easily, it would prove difficult to aim the pen while holding it next to the ball before triggering it to send the ball along the desired path.  Remember, this would be performed while the demonstrator and the ball were free-floating, subject to air currents set up by the ventilation system.                                               

The resulting actuator uses the vacuum created by suction on a tube to hold the ball against a flexible cup.  The ball compresses a coil spring protruding from the center of the cup.  Thus captured, the ball may be aimed accurately so that it will follow the desired path in front of the cloth metric measure strip that will be Velcro attached  to the 4'x 6' backdrop affixed to the mid-deck locker doors to improve visibility of objects during filming.  Using two different springs and the vacuum system the teacher can release the spheres at the same time, using the same force repeatedly.                                                                                                                       

Ball point pen retractors or something similar  may be used  in 1 g on  a  billiard ball and ball bearing sitting  on a level table  or on a V-groove track to duplicate  this activity in the classroom. 

EFFERVESCENCE

 

Click on link below to go directly to the Lesson Plan:

 

EFFERVESCENCE LESSON PLAN

The goal of the effervescence activity was to understand why products may or may not effervesce in a microgravity environment.  The object was to show the action of bubbles produced in a microgravity environment and to observe the lack of buoyancy.  The activity originally  called for a clear plastic container, open on top, an effervescent tablet, and a water gun.  The teacher would have placed the tablet in the container, then used the water gun to add water.  This scenario presented several concerns to the safety board and engineers.  Though one of the Skylab crews demonstrated that water could be squirted .into an open container using their food re-hydration water gun, they had good control of the forces acting on the water, i.e., the release of liquids into the cabin.  Errant fluids pose a threat to electronic systems in the Orbiter.   The container would have to be covered. Glass containers were undesirable due to possible breakage.  The search began for transparent bottles of adequate size, clarity and acceptable material.            

A standard drink container with a tablet sealed inside was tested.  Filming the action was difficult, and the pressure generated by the carbon dioxide gas caused the water to be ejected from the septum.  Some means had to be developed to accommodate the CO2 and allow for air displacement during filling in cases in which a hard walled Plexiglas container was considered.   Finally, a transparent lexan bottle was discovered that proved to be the solution to this and other hardware puzzles.  Lexan is tough, transparent, and flight approved. There would be no concerns about off-gassing or breakage.  Pressure tests proved the bottles able to maintain a seal to at least 60 psi, and the tablets generated somewhere in the range of .2 psi.                                                

Modifications on the bottle include the addition of a Teflon gasket in the lid, and a viton diaphragm glued over the mouth.  The diaphragm has a slit to accommodate insertion of the effervescent material, and functions as a barrier for the water while the lid is off.   The water in the bottle is colored with blue food coloring to enhance visibility. 

Picture of Christa inserting the tablet into cap-slot

Photo is of Christa screwing on lid while tablet effervesces

The last component of this activity to be discussed is the effervescent tablet.   A commonly available tablet will be used, but it will be crushed and the powder enclosed in water soluble gelatin capsules that may be purchased at a pharmacy.  The capsule is perforated by 60 holes. 

Several concerns led to this arrangement.  The first was safety.  It is not as simple to insert an unprotected tablet through the slit in the diaphragm as one might believe.  The small amount of water that will be present on top of the diaphragm when the lid is removed  begins to dissolve the tablet immediately allowing water to escape, and preventing observation and filming of the object.  That portion of the tablet that enters the bottle then reacts quickly so that observation and study are hindered.  It is hoped that the perforated capsule will allow the desired results to be achieved while slowing down the reaction time of the chemicals.  

 

 

CHROMATOGRAPHY

Click on link below to go directly to the Lesson Plan:

 

CHROMATOGRAPHY LESSON PLAN

The objectives of this activity were to demonstrate chromatographic separation of pigments and capillary action in microgravity.  This activity was originally part of the hydroponics demonstration, thoughin that case, capillary action and osmosis would have been observedinstead of chromatographic separation.  The original plans were changed primarily because of the complexities they created in thedesign of the hydroponics chamber.  Time was a critical factor driving the selection of off-the-shelf equipment and design, testing, andfabrication of all the hardware for this project.  Thus, a chromatography activity emerged.         

Chromatography in Space Lesson

Tests with various inks, papers, and quantities of water promisedthis to be an easily duplicated demonstration for the classroom.  Place a spot of ink on a piece of paper, hang the paper on thebulletin board, add a drop of water, and observe while the waterdissolves the ink.  The water moves against gravity due to capillaryaction, carrying the components of the ink with it.  These componentsare deposited in layers or strata, much like sediment in a river,according to their molecular mass and the size, shape, and chargeof their molecules.

The teacher will use strips of filter paper 1/2"x 3" long, and aflight approved, water base ink felt tip pen.  The paper will beplaced in a lexan vial after adding a water drop to begin the process.  This prevents evaporation from slowing down and stopping theprocess prematurely.                                                                                                

There are parallels between the behavior of the ink molecules in this demonstration and the behavior of the molecules of the chemicals used in the continuous flow electrophoresis (CFES) used to process pharmaceuticals.

SIMPLE MACHINES 

 

Click on link below to go directly to the Lesson Plan:

 

SIMPLE MACHINES LESSON PLAN
      

The objective of this activity was for students to understand similarities and differences between the use of simple machines in space and Earth environments.  The question posed was "would certain simple machines have been developed by people who always lived in microgravity?"  Stated another way, “what are the applications in space for simple machines like the wheel and axle, lever, inclined plane, wedge, and pulley?”                

The original plan called for a wooden inclined plane, a cart with four wheels, hammer and nail, screw to be screwed into the inclined plane, and a pulley.  The commander immediately vetoed the idea of driving nails into the wood because of the potential for damage to the Orbiter".  A refresher in physics reminds one that the forces input into the hammer-nail-wood system would ultimately have to be transmitted to either a crewmember or the craft. Since the goal of this particular part  of the activity was to use the hammer to pull the nail, thereby demonstrating a fulcrum and lever, it was decided to  demonstrate the lever using the 18" pry bar in the Orbiter tool kit instead. Also, it was not desirable to use wood due to flammability. For some time a 4”wide folding aluminum meter measure was considered to serve as an inclined plane and with the Newton 's Laws demo, but it proved to be a stowage problem. A wedge of aluminum 10” long x 2" wide x 3" high was produced to serve as the inclined plane and wedge.  It also was drilled and fitted with an insert to provide friction for a screw that the teacher will use to demonstrate the use of a simple tool, the screwdriver, in space.   

A pulley will be attached to the mid-deck locker and used to pull a small car "up" the inclined plane. This demonstrates that the wheels are useless on the car, lacking friction with the plane, but that the wheel functions well as a pulley to change the direction of a force.  Of course, multiple pulleys could be used to multiply a force to assist in moving mass in microgravity.

 

Back to the Table of Contents

 

For added information or copies of the project, contact the project editor Jerry Woodfill, at ER7, NASA JSC, Houston , TX 77058 .  Phone: 281-483-6331,  E-mail: jared.woodfill-1@nasa.gov

 

The project is a work of the Automation, Robotics, and Simulation Division of the NASA Johnson Space Center , Houston , Texas . As part of the Space Educators’ Handbook, its ID identifier  is OMB/NASA Report #S677.