Virtual Skies

Aviation Research You Decide

Step 1
Questions Question 1 Question 2 Question 3 Question 4
A.   Decision to be made(Phrased as a question.): How will the vehicle take off, taking advantage of research in efficient propulsion and smart materials? How will the wing(s) appear, taking advantage of biomimetic research? How will the vehicle dock? What smart materials can help?
What features will be noted on the drawings, other than those referenced in questions 1, 2, and 3?
B.   Critical Factors Involved

Propulsion Research

Current propulsion use

Smart materials

Limits provided by atmosphere, weight, and reusability

Propulsion for high-speed exit of atmosphere.


Current wing design

Biomimetic Research

Wing design research

Smart materials

Wing use for descent

Geometry of dock at international space station

Geometry of dock at satellites

Using tethers for docking

Smart materials

Fine-tuned propulsion / steering for docking


Capacity for people, cargo

Weight requirements

Characteristics so can be reusable

Steering devices

Take-off and landing gear

C.   Information known

New research indicates that a new shuttle could take off as well as land like an airplane (based on recent high-speed achievements).

No air in space, so wings and propellers useless! Also very cold, density is zero, and low pressure (could these be indicators for smart materials involving propulsion?)

Propellers produce much thrust needed for vertical lift in takeoff, while wings provide lift for horizontal movement. X-class aircraft take advantage of this.

Pathfinder airplane uses solar energy to produce electrical energy to fuel engines that turn propellers all along length of wing.

Propellers can be driven by human force (turning gears on a bicycle).

Turbines rely upon high-pressure, quickly moving gasses to produce more thrust.

Ramjet engines work as turbines do, but high-speed air is rammed into engine (for pressure), so it is ideal for high-speed aircraft but not useful in low-speed craft.

X-15 airplane uses rockets at take-off until air is fast enough to effectively make ramjet work. Then rockets disabled and ramjet works on its own.

Rocket carries all of its own oxidizer (oxygen) and fuel. Doesn't use external atmosphere, so functions in any environment.

Solid rockets must be exhausted (no turning off before fuel is gone), while liquid rockets can be stopped as needed.

Ion / Solar-Electric Propulsion: solar energy fuels electric generators that charge ions moved as high-pressure gas out of engine. Fueled with xenon, which is an abundant resource. Very slow to accelerate. 83 kg xenon gives 2.5 kW or 3.4 horsepower in one year.

Space Tethers: Spacecraft is attached to satellite or space station, which moves it about itself, then releases it appropriately, in the right new direction. If tether is conductive, as it passes through differing magnetic fields, it would create electricity. Tethers reaching into Earth's atmosphere could be used to propel objects into space or from space back to earth.

Laser / Solar Sails: Light produces force, so focussed light (lasers with lenses) could produce wind in sails. 10 gigaW laser for 16-gram vehicle.

Space elevators: A floating tower that moves in Earth's orbit could help move things from Earth to space with elevators along the tower. Would be very expensive to begin construction.

MR Fluid used for noise reduction by creating friction damper. Could be effective to quiet propulsion?

S-M Alloys have been used in smart rotor for helicopter, where rotors are easily tunable.


Airplanes have wings with several control surfaces and moving parts; new wing design uses smart materials to limit moving parts and make control surfaces only present when needed.

Wing should be straight for good lift & stability at slow speeds, then sweep back at high speeds (swing-wing design).

Area is related to lift, so high-area wings important after stability achieved (delta wing).

On rockets, no wings upon descent, just parachutes attached to the nose cone.

Fins or wings needed on rockets to help stabilize, especially early in take-off.

Biomimetics involves using natural design ideas to create product with multifunctional components.

Wing design research focuses on smooth wings and fins made of flexible materials, that can move between configurations to supply movement.

Several miniscule fliers have been created with smart materials, often based on insect flight because of great weight-lift ratio.

Smart materials respond to heat, electricity, and magnetism. They are very reliable, have low power requirements, are fast-acting, and highly controllable.

Piezoelectic Materials require input of voltage to change shape, or change of shape creates electricity. Current research uses a piezoelectric actuator to change wing and fin shape, for swimmers and wings that don't have external moving parts, are stronger, and more efficient in movement.

Shape-Memory Alloys change shape (to remembered shape) in response to temperature. Used in walking, swimming, slithering, and flying robots.

Atmosphere varies in pressure, temperature, and density with altitude. These changes could trigger change in aircraft to new wing orientations to take advantage of best modes of flight. Rotors for take-off with straight,܍ `Un!Qx;>a6We=Z0*|سWv1~7, V_@ q9k}\qW nK,aEhcE jX xȻ` ŀ ! ,qA*D"AȷP%*D9X(L8e͈~"r@a݄2cC:Oޥ!-Šy*nPyl>+tGʲB[N\V#RH$$%{U^Uj.TY+O⫩ttex͆e_"8,cz]шMo)H0.MEIrxPlud]@W+@C8sD[yi%H{m~ٹb $FmL$t4#uMɚ3s{)Tnv, *bW$vz 7c;QP*}tVܝTcLFD"ʸhT=/VeDH0UI%9Ȑ&AQ%EۣPdr$P*M0IgʪG27&Rs@)zQ&jqpM/L1?) tu dڊ>ѵnbT*{-r,x>Ю[.GP۶!u>W*S vDn_>߶JV DYsB15P/,<"$8{sDn`1O7^]'V wMnIJ@Gϒۃϧٽ+}fi:Vx2[)GԪYt`f A2+([.*+X+Oɢ).|DNb_a*8FlׁNEZPg WJ҉rZd3LPΙQVC39*"'|-i"+D?L;3VVa4I֒5F4^ HͭôGr5AkVwHc(2#gxhPDuO/H{=kFx9U]a-'GVϋN rB0#:&\`OgGI`KN9lVB .ӢECCLݷm.Lvj7%}ug8jސ1,tb$9vls\vBюi܌_r\h+@25U%VB,GevGo"[Qry"W*12Zm.L 3%umZv .'ˎEsZ-pZ``5HĭqŹ> Q+xp칮}?$G[nݻ07$\5c.@+$:g?70W'>IJxF0i$N=O> -<[}*p:m8N1\-[!ǖ#9H&WLJԌPu~iNX"Y}U"mYN|ɫ}A>iۖxFK=8߹)>܁nOl^aCy%YzVt(yK!sszDZQ=SS?p@&9cN=V[ۛaGOJ$p>(yV/ۘ`AlU Q VkvvɎPr;I=9 `xWW5F"DuLT"ND+:@1qXGM|º-GࣸӮ/BΪ3BLgB11e=K wX\Hq+m E[V3hE0iweTLvuD,f^f9pB'1̷i;b{e\^վqARiۚY~m}c )yAl1 }{m[e-;ޛ}_.Wl\r  G>*?}%$bm嫬/!R-mNZc2 eDAYn6!%lA߷:.{t㓢1c?\tm݅`[J^Fic+B٩I͵BM@eX8<K &VW!48#s)TW-۸;x,m qWj'@f\G#p3V-`O!JbiZMlFb h<Bx]ԩ#y~x6.{OR-ȃ9pcM5o'R7AT5J0ժb.y r~iVLhRq#wT튝RsXuY I9 MȞ@Ow6Nld>UwOIcu@TAzg̓bAۮ VZ-[T#KTƕ9Y,?1+5 $t tZ?tY%;q,*N 1V[pl&osn"zv}gqhθzedA:쭛# >+-oW9*a/- Ie=ڑ*LR7IWym G҇0U&㒣rQ :;2|1/ot:uZz9mqe= /R:z>e?t9WdτhbNRx⹦\F8Qcۯ^[?p1+Y<׊jBp&2H/Cf 8Mtgt /bxd$p8pR$SP cf+@")F P'K(ȿjF9Z66 eEO2Tl)! Ua fR4#mwZW&~MmxkA6e;D;]Mz3?FWسsCj<;Glr`fC!Niyih^'. Jk|BЮ 7Ps}ӑvn|/H ī-еi! A <թJp4~2-{-| m 8]+w߷vf ebzI!">~8#$-&Yb˞ݘvdFR#n>=&Aj{vۉL.3z훉ݣ,m]ݟBܧ  +rǼĒmpgXY9θ!..nܹ#) j86oVn:-v'9HNVN 8w?gIBh  *i ;Ͽ7tdC~(^auHcLv[{c^_ΨʢK&]=1iGL$3-쑔2cШfKLmVM'PXHPp C@B4@*Ȫa2Q8A!zѻmx\;r pPsf,a=> q"$XʄrQ#BFzKpØTlӘOb 7 ] |f\*#BHAbq /5Ғyuz=RI!4hI Ź:,gl+ڼ ʅN:حn,Y(URwVCqjq,pQ]s:@J@䫄 h0 2zpR?AUHi*HHi8& jF) ` Ʃx څB7!rNq=RNX(A$M":Ivv+44Iۍ cV:"ց 3X䎛1ICf]3d1α/Գ^ku˶#ݍ+OX)@45=q4+pff` 2'aN1a[m]pн;6΀%8qNZ/!'`jIG= .H:\uOq[;qsp#u G*k攜;#zLCTzx"&^^*g }B!_fnoJzAZh&)6~Hg&2<0U Nҹ@Eb#-C#LF/,b"IUsN7n=joLtȸ4ۀaõ9pVe WIBq? K\}Fԩs?8Idan/98"k1 Apj%=$s'jsYc_,ӓ-&$Є B yUyT!!B`!HH [ B|~lo dFNeFOR"!2 ţՉTvw=8,-ȹe8CjzYMrz7#n: p<ְt[犛+6-VR-Ve=1jk%蘨⬷{ .$lDŦB :)/JwEsZR*֣CG`F1=0!0E\xLCCB-^4sj\K bbjIxQ"R#MX+br< =F<XW2zLc8iP Jv>_V@P,8U` @!Wop/`NT!?$=TQQ% dj@M*;l J8x7% ૵1(D?C+c~jpS %Uj1ZF]Hy~aypC8o`kť5gLr8~\MDK ';$"@N&*ݽ plVn;N25̣(ڻG-$3> x;-FC[no]{XbGnTzs#ogrmL],QcVm1l3\w۸nɕ{op{Wk~<RzXȷmM!_w4j^wR6zzk)yTI`!!@Bz [`ыٷLD#YJb۩1ջ"Diq#WJP@m, with aircraft components for landing (like space shuttle)

Take off loudest

Fuel tank destroyed and rocket boosters may be damaged in parachute landing.

Weight very heavy, with all fuel stored in tanks - MAY EXCEED REQUIREMENTS.

Fuel is not environmentally friendly, reusable.

Take off requires several miles of clear space.

Traffic may be difficult to control and monitor.


Most parts reusable.

 

3. Rocket-style propulsion system only

Take off loudest

Most parts not reusable.

Weight very heavy, with fuel all stored in tanks-MAY EXCEED REQUIREMENTS.

Fuel is not environmentally friendly, reusable.

Traffic may be difficult to control and monitor.


Take off requires several miles of clear space.

Only nose cone reusable.

 

4. Aircraft-style propulsion system with "smart" wings that uses ionic propulsion at 350,000 feet

Take off loud and requires horizontal space.

Acceleration very slow.

Traffic may be difficult to control and monitor.

All parts reusable, including very sturdy ionic engine

Weight very light; ionic propulsion uses relatively light fuel(xenon & solar energy) very efficiently.

Solar power is always obtainable, environmentally friendly.

See "smart" wing pros/cons below.


 

5. Aircraft-style propulsion system with "smart wings" that uses sail at 350,000 feet

Take off loud and requires horizontal space.

Currently, a tremendous amount of energy is required to generate the laser to "push" the sails. This means a high weight of fuel for generating energy to make the light.

Deploying sail could be complex, error-prone procedure.

Traffic may be difficult to control and monitor.


All parts reusable (except sail?)

Weight could potentially be very light, as fuel could be harnessed solar energy.

Sail travel could be very fast.

See "smart" wing pros/cons below.

 

6. Aircraft propulsion system with "smart" wings that uses space tethers at 350,000 feet. Aircraft will have ionic, rocket, or sail-powered propulsion for subtle travel changes.

Take off loud and requires horizontal space.

Limited to using only previously tethered "stops", unless a means for tethering from space craft is developed.

Miscalculations from angle and time of release from tether could cause space craft to be misguided.

Movement of people and cargo from space craft wS'U؃uuAE+ uC[TtWBz%"h*T !Wh#? !.4n5#)Fı(3(yN b\bH+^S#攀esOm(*pNdJ`0XML[3pGp%F]ԁ?yFA*va ]<%+Zmщ8БO,p @ :/Vi4tqcorDNd?ډHh57 yXDN@ yNec")I8f1+9jq0yZ&蝻f8Xoc]#R\bMrFtXԲ+^WPd:qL 6m8.%(Q(B_BcVoK_)~܎s+>k\c9aeErcˀBGAm[ G@#|[>_?;ц}HB/8sL\ԝ40.Bu)Oa~o,R?,0f$i ൌ?BK,sf^8'ߗ$P*:~|]|d-4?[)-#:x?\~!# Spaceward Bound - Australia 2009

 National Aeronautics and Space Administration + NASA Quest
+ Search Quest
+ NASA Ames Education
 Find it at NASA

Less moving parts

Lighter and less bulky than traditional wings.

No risk of hydraulics leaking.

Wing is flexible and has better structural integrity.

Wing is multifunctional and can alter its shape to increase surface area, cant, and location of leading and trailing edges.

Steering components could be present only when needed; hidden to make vehicle more aerodynamic when not in use.


 

C. DOCKING

     

1. MR Fluids to dampen contact- fluid would be in liquid state during cruising and docking, then become solid after docking, to create a rigid seal with dock.

Electric/Magnetic fields at docking stations would need to be controlled to prevent failure of MR Fluid.

Electric/Magnetic fields would need to be focussed to prevent negative interaction with magnetized data like that on computers.

Fluid would soften impact on otherwise breakable, bendable parts.

Fluid could allow for good seal with docking ports of different shapes and sizes (Fluid molds to proper size).

Docking portion of vehicle would be difficult to damage due to its flexibility during flight.

Displacement from dock is safe and convenient.


 

2. Ionic or Conductive Polymers for locking ship to dock. Vehicle docks in a stable manner, then water floods the seam of this docking. Water and electricity activates the polymers at both ends of the dock, to cause them to change configuration to lock into each other tightly.

Not useful on docks not previously designed for this locking.

Electricity required may drain energy resources; there are more efficient mechanical means.

Electricity and water may cause significant threat to electrocution.


Water leakage indicates lack of success of locking (serves as a vital component for locking and as a testing variable).

Polymer binding is very strong and tight.


 

3. Piezoelectric Materials for sensing position, subtle changes

Piezoelectric Materials do not tend to be very mechanically durable, and there is some difficulty coupling piezoelectric material to other structures.


As pressure against piezoelectric sensor occurs, current is generated that fuels subtle changes by engine/ steering to alter position.

Vehicle can dock with high precision while on "auto pilot."

Piezoelectric Materials can be made easily for any purpose, with any composition and shape.


 

D. OTHER TRAITS

     

1. Shape-Memory Alloys for heat defense; alloys would alter shapes to create for reflective or effective boundary from heat.

Alloy sheets will need to be bound to vehicle in a way so they don't move / fall off, making heat damage due to exposure more of a risk.

Heat from reentry into atmosphere can be harnessed to help prevent heat-damage inside vehicle.

Shape-Memory Alloys can tolerate strain 3 to 25 times higher than piezoelectrics can.


 

2. Magnetostrictive Materials for new tank / cargo space design (collapsible empty space)

A mechanism for changing the entire region's magnetism would need to be designed, without interfering with computers and other magnetic-dependent structures.

Regions near joints would have to be flexible, to tolerate the compression / expansion of the walls of the vehicle.

Magnetostrictive Materials are not easily embedded in control structures.

Areas containing empty space could collapse and expand appropriately, making vehicle the ideal size to increase wing area: weight ratio.

Magnetostrictive materials can undergo a larger range of temperature, strain, and input voltages than electroactive polymers can.

If the walls of the vehicle are strained, they will create current, which can be used to either alter the walls with respect to the strain, or alter the course of the ship (see Docking #3 above).


 

3. Streamlined and smart airplane skin, with de-icing capability (shape memory alloys)

Addition and maintenance of sensors may be expensive and labor-intensive.

Deicing is efficient and easy to monitor, without human labor being exhausted.

State of airplane surfaces can be continuously monitored, so maintenance can be made efficiently

Airplane surfaces will be streamlined and in optimal performing status at all times.

Shape-Memory Alloys can tolerate strain 3 to 25 times higher than piezoelectrics can.

See Wings #4 above.


 

4. Shape memory alloys for brakes

 

Brake heat can be used to expand the surface area of the braking pad, making braking more efficient.

Brake heat is harnessed, rather than allowed to expaave limited supplies we did have the advantage of plenty of good beef on hand. Later, David and I lived in Gove and Darwin after Cyclone Tracey and even then fresh supplies were limited compared to southern states.

In addition I have had many years been cooking for Scouts fund-raising events and a hundred and one sausage sizzles so I can find my way around a cooktop. I hope to give everyone good food so that you can enjoy your work.

Finally, above all, I am looking forward to meeting everyone and joining in the discussion on making science relevant to all school students.

 FirstGov  NASA


Editor: Linda Conrad
NASA Official: Liza Coe
Last Updated: April 2007
Teachers Contact: Liza Coe
  (Lizabeth.K.Coe@nasa.gov)

 Spaceward Bound - Australia 2009
 National Aeronautics and Space Administration + NASA Quest
+ Search Quest
+ NASA Ames Education
 Find it at NASA

2. SMART WINGS

Smart materials allow the wing to be simple with few moving parts, while also allowing it to change dynamically. As the aircraft speed increases, the wing area can increase to work more efficiently. Wing direction would also change, to go from a straight to delta design.


Wing steering controlled with piezoelectric actuators can reduce wing weight, simplify the wing, and improve flexibility and strength, while creating a structure with multifunctionality. The wing could be changed along its leading and trailing edges, in terms of cant and area, to more efficiently steer the vehicle. Potential issues include focussing of electricity for each actuator and coping with electric storms.


These sensors could help the pilot and machines in the vehicle monitor effects of wind and weather on the vehicle surface, and change flight traits based upon this. Flight becomes more efficient based upon these changes, although it may be difficult to determine between different external forces and electrical storms near the vehicle could cause problems.


 

3. DOCKING

MR Fluids to dampen contact; fluid would be in liquid state during cruising and docking, then become solid after docking, to create a rigid seal with the dock

Piezoelectric sensors could be used for steering situations (like docking) requiring high accuracy. The sensors could directly communicate with engines on the vehicle to subtly change position. Durability of sensors is the only concern with this design.

Water helps to check the seal produced during locking, as well as providing stimulus (with energy) to get electroactive polymers to re-shape and seal together. However, the water/electricity interaction could be hazardous, if not monitored. This method could only be useful on docks with previously attached electroactive locking devices.


 

4. OTHER TRAITS

MR Fluids could help reduce noise and vibration during flight, while providing some stress relief for joints of the vehicle when structural integrity is not crucial.

Brakes at the K-12 level, but my work incorporates place-based education at the college level.  Scientists and teachers will be invited to interact with local experts while we are in the field.

Dr Adrian Brown

Planetary Scientist,
NASA Ames Research Center

Multispectral and hyperspectral instruments such as TES, THEMIS, CRISM, and OMEGA are essential tools in the mapping of the surface mineralogy of Mars. My planned SBA research activities will revolve around remote sensing of