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Advanced Certification Study Guide TRIPOLI ROCKETRY ASSOCIATION, INC.

Advanced Certification Study Guide

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Advanced Certification Study Guide. TRIPOLI ROCKETRY ASSOCIATION, INC. Which of Newton’s Laws best describes the behavior of a rocket motor?. Newton’s Third Law: To every action there is always an equal and opposite reaction. - PowerPoint PPT Presentation

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Page 1: Advanced  Certification Study Guide

Advanced Certification Study Guide

TRIPOLIROCKETRY ASSOCIATION, INC.

Page 2: Advanced  Certification Study Guide

Which of Newton’s Laws best describes the behavior of a rocket motor?

Page 3: Advanced  Certification Study Guide

Newton’s Third Law: To every action there is always an equal and opposite reaction

Page 4: Advanced  Certification Study Guide

How does Newton’s Third Law “To every action there is an equal and opposite reaction” relate

to rocketry?

Page 5: Advanced  Certification Study Guide

That a rocket flies because the rocket motor “pushes” the rocket in a direction opposite the

exhaust jet

Page 6: Advanced  Certification Study Guide

What are the three forces acting upon a rocket during the course of its flight?

Page 7: Advanced  Certification Study Guide

Gravity, thrust and aerodynamic drag

Page 8: Advanced  Certification Study Guide

What are the major factors that determine the maximum altitude of a high power rocket in

vertical flight?

Page 9: Advanced  Certification Study Guide

Motor thrust, weight, and aerodynamic drag

Page 10: Advanced  Certification Study Guide

For an inherently stable rocket, what is the relationship of center of gravity (CG) to the

center of pressure (CP)?

Page 11: Advanced  Certification Study Guide

The CG must be forward of the CP relative to the desired direction of flight

Page 12: Advanced  Certification Study Guide

A 4” diameter rocket with its motor is determined to have the center of gravity (CG) four inches behind the center of pressure (CP). Is this a stable rocket?

Page 13: Advanced  Certification Study Guide

No, the CP must be behind the CG for the rocket to be stable

Page 14: Advanced  Certification Study Guide

The center of pressure (CP) of a rocket is generally defined as:

Page 15: Advanced  Certification Study Guide

The point at which aerodynamic lift is centered

Page 16: Advanced  Certification Study Guide

What is the “rule of thumb” for a stable rocket?

Page 17: Advanced  Certification Study Guide

That the center of gravity (CG) is one body diameter in front of the center of pressure (CP)

Page 18: Advanced  Certification Study Guide

When determining the center of gravity (CG) of a rocket with a heavier motor at the launch site,

one can:

Page 19: Advanced  Certification Study Guide

Install the motor, recovery system and payload and determine the balance point of the rocket

as it is ready for flight

Page 20: Advanced  Certification Study Guide

What happens to the center of gravity (CG) of a rocket during a solid rocket motor’s thrusting

phase?

Page 21: Advanced  Certification Study Guide

The center of gravity (CG) shifts forward

Page 22: Advanced  Certification Study Guide

How can a statically unstable rocket be made stable?

Page 23: Advanced  Certification Study Guide

Adding weight to the nose

Page 24: Advanced  Certification Study Guide

What are the three methods used to shift the center of gravity (CG) of a rocket forward?

Page 25: Advanced  Certification Study Guide

Add weight to the nose, make the rocket longer, use a smaller (or lighter) motor

Page 26: Advanced  Certification Study Guide

What are three methods used to shift the center of pressure (CP) aft?

Page 27: Advanced  Certification Study Guide

Make the rocket shorter, use larger fins, increase the number of fins

Page 28: Advanced  Certification Study Guide

What is the definition of coefficient of drag (Cd)?

Page 29: Advanced  Certification Study Guide

A dimensionless number representing the rocket configuration, Mach number, and angle

of attack

Page 30: Advanced  Certification Study Guide

What happens to the coefficient of drag (Cd) as the rocket approaches the speed of sound?

Page 31: Advanced  Certification Study Guide

The Cd increases

Page 32: Advanced  Certification Study Guide

For a subsonic rocket, what major factors affect the coefficient of drag (Cd)

Page 33: Advanced  Certification Study Guide

Speed, airframe dimensions, nosecone shape and fin shape

Page 34: Advanced  Certification Study Guide

What effect does a boat tail have on a subsonic rocket’s coefficient of drag (Cd)?

Page 35: Advanced  Certification Study Guide

It decreases the Cd by reducing the base drag

Page 36: Advanced  Certification Study Guide

The flight of a high power rocket can be seperated into three portions; they are:

Page 37: Advanced  Certification Study Guide

Powered flight, un-powered ascent and descent

Page 38: Advanced  Certification Study Guide

What is the thrust curve of a regressive motor burn?

Page 39: Advanced  Certification Study Guide

A regressive burn has a high initial thrust relative to the ending thrust of the motor

Page 40: Advanced  Certification Study Guide

What is the thrust curve of a progressive motor?

Page 41: Advanced  Certification Study Guide

A progressive burn has a lower initial thrust relative to the ending thrust

Page 42: Advanced  Certification Study Guide

Why does a bates grain have an essentially neutral thrust curve?

Page 43: Advanced  Certification Study Guide

Because the burn area of the motor remains relatively constant

Page 44: Advanced  Certification Study Guide

What is the function of a motor liner and the O-ring seals in a solid rocket motor?

Page 45: Advanced  Certification Study Guide

To keep the hot gasses of the motor from burning or melting the motor case

Page 46: Advanced  Certification Study Guide

What is the most common oxidizer in commercially available high power composite

solid rocket motors?

Page 47: Advanced  Certification Study Guide

Ammonium Perchlorate

Page 48: Advanced  Certification Study Guide

What is NH4ClO4?

Page 49: Advanced  Certification Study Guide

Ammonium Perchlorate

Page 50: Advanced  Certification Study Guide

A small hole is typically recommended near the top, but below the nosecone or payload section, of a high power rocket’s booster section. Why?

Page 51: Advanced  Certification Study Guide

The hole vents internal air pressure as the rocket gains altitude to prevent premature

seperation

Page 52: Advanced  Certification Study Guide

What happens when changing to smaller or fewer injector orifices in an ideal hybrid rocket motor (assume the oxidizer weight stays the same)?

Page 53: Advanced  Certification Study Guide

The total impulse stays the same and the average thrust decreases

Page 54: Advanced  Certification Study Guide

What happens when changing to more or larger injector orifices in an ideal hybrid rocket motor (assume the oxidizer weight stays the same)?

Page 55: Advanced  Certification Study Guide

The total impulse stays the same and the average thrust increases

Page 56: Advanced  Certification Study Guide

What is the oxidizer most commonly used in a commercial hybrid rocket motor?

Page 57: Advanced  Certification Study Guide

N2O, Nitrous Oxide, commonly called NOX

Page 58: Advanced  Certification Study Guide

What is the nominal tank pressure of a nitrous oxide hybrid motor at 75* F?

Page 59: Advanced  Certification Study Guide

750 psi

Page 60: Advanced  Certification Study Guide

Above what temperature does pressurized nitrous oxide change to a gas?

Page 61: Advanced  Certification Study Guide

97*F

Page 62: Advanced  Certification Study Guide

A rocket with a motor cluster consisting of a central composite motor and four black powder motors

using thermalite igniters or electric matches:

Page 63: Advanced  Certification Study Guide

Will result in the black powder motors starting first followed by the central composite motor

Page 64: Advanced  Certification Study Guide

What typically happens to a marginally stable rocket with a hybrid motor during the thrusting

phase?

Page 65: Advanced  Certification Study Guide

The rocket may become less stable

Page 66: Advanced  Certification Study Guide

In general terms, the specific impulse of a rocket motor is:

Page 67: Advanced  Certification Study Guide

The total impulse divided by unit weight of propellent

Page 68: Advanced  Certification Study Guide

In general terms, the total impulse of a rocket motor can be described as:

Page 69: Advanced  Certification Study Guide

The product of the average motor thrust and its burn time

Page 70: Advanced  Certification Study Guide

The average thrust of a rocket motor is 100 Newtons and the burn time is 4 seconds. What

is the total impulse?

Page 71: Advanced  Certification Study Guide

400 newton-seconds

Page 72: Advanced  Certification Study Guide

Which motor has a higher total impulse?

J200J400K200

Page 73: Advanced  Certification Study Guide

K200

Page 74: Advanced  Certification Study Guide

Which motor has a higher average thrust?

J200J400K200

Page 75: Advanced  Certification Study Guide

J400

Page 76: Advanced  Certification Study Guide

What is the difference between a J640 and a J320 high power rocket motor (assume full 1280

Newton-second J motors)

Page 77: Advanced  Certification Study Guide

The J640 burns out twice as fast as the J320

Page 78: Advanced  Certification Study Guide

Which of the following has a total impulse in the J motor range?

It = 600 Newton-secondsIt = 1000 Newton-secondsIt = 1290 Newton-seconds

Page 79: Advanced  Certification Study Guide

It = 1000 Newton-seconds

Page 80: Advanced  Certification Study Guide

What is a Newton?

Page 81: Advanced  Certification Study Guide

The amount of force required to accelerate on kilogram one meter per second per second

Page 82: Advanced  Certification Study Guide

What does the motor designation I220-8 mean?

Page 83: Advanced  Certification Study Guide

The motor is in the I impulse range with an average thrust of 220 newtons and an 8 second

ejection delay from the motor burn-out

Page 84: Advanced  Certification Study Guide

What is the difference in kinetic energy between two identical rockets, one descending at 30 feet per second, the other descending at 60 feet per second?

Page 85: Advanced  Certification Study Guide

Four times as much energy

Page 86: Advanced  Certification Study Guide

The equation for determining the energy of a moving body (such as a rocket) is:

Page 87: Advanced  Certification Study Guide

E=1/2mv2

Page 88: Advanced  Certification Study Guide

What is the purpose of a launch rod, rail, or tower?

Page 89: Advanced  Certification Study Guide

To keep the rocket pointing in the right direction prior to flight AND to control the rocket’s flight

long enough to allow aerodynamic stability

Page 90: Advanced  Certification Study Guide

What is the purpose of a launch lug?

Page 91: Advanced  Certification Study Guide

To guide the rocket along the launch rod or rail

Page 92: Advanced  Certification Study Guide

A rocket with a motor cluster consisting of a central composite 54mm J415 motor and four 29mm G80 composite

motors using thermalite igniters or electrical matches:

Page 93: Advanced  Certification Study Guide

Will result in the G80s starting first followed by the J415

Page 94: Advanced  Certification Study Guide

What can happen if all the motors of a cluster do not ignite at launch?

Page 95: Advanced  Certification Study Guide

The rocket may not fly straight

Page 96: Advanced  Certification Study Guide

What is a shred?

Page 97: Advanced  Certification Study Guide

A failure of the rocket airframe during boost resulting in destrtuction of the rocket

Page 98: Advanced  Certification Study Guide

What is a cato?

Page 99: Advanced  Certification Study Guide

A failure of the motor causing flight termination

Page 100: Advanced  Certification Study Guide

What is the primary requirement for a rocket motor igniter?

Page 101: Advanced  Certification Study Guide

It must transfer sufficient heat to the propellant to assure ignition

Page 102: Advanced  Certification Study Guide

What is covered in the scope of NFPA 1127?

Page 103: Advanced  Certification Study Guide

Design and construction of commercial high power rocket motors, high power rocket

vehicles and launch operations

Page 104: Advanced  Certification Study Guide

The design and construction of high power rocket motors, high power rocket vehicles and

launch operations is detailed in what code?

Page 105: Advanced  Certification Study Guide

NFPA 1127 and the Tripoli Safety Code

Page 106: Advanced  Certification Study Guide

Individuals, firms, partners, joint ventures, corporations or other business entities engaged in high power rocketry activities are exempt from NFPA 1127 until what point?

Page 107: Advanced  Certification Study Guide

When selling to qualified users in conformance with NFPA 1127

Page 108: Advanced  Certification Study Guide

Who is exempt from NFPA 1127?

Page 109: Advanced  Certification Study Guide

Federal, state and local government, colleges, universities and license for-profit businesses

engaged in high power rocketry activites

Page 110: Advanced  Certification Study Guide

What is the purpose of NFPA 1127 and Tripoli Safety Code?

Page 111: Advanced  Certification Study Guide

Provide safe and reliable motors, establish flight operations guidelines and prevent injury

Page 112: Advanced  Certification Study Guide

What is the Authority Having Jurisdiction?

Page 113: Advanced  Certification Study Guide

The organization, office or individual responsible for approving equipment, an

installation or a procedure

Page 114: Advanced  Certification Study Guide

What is a complex high power rocket?

Page 115: Advanced  Certification Study Guide

A rocket having more than one stage AND a rocket having a cluster of rocket motors

Page 116: Advanced  Certification Study Guide

What are the rocket motor criteria (minimum) that defines a high power rocket?

Page 117: Advanced  Certification Study Guide

A rocket with a single motor with more than 160 Newton-seconds total impulse or an installed impulse of 320 Newton-seconds and no more than 40,960 Newton-seconds AND a rocket with a single

motor having an average thrust in excess of 80 Newtons

Page 118: Advanced  Certification Study Guide

What is the lower weight limit of a high power rocket?

Page 119: Advanced  Certification Study Guide

A rocket weighing more than 53 ounces

Page 120: Advanced  Certification Study Guide

When is a recovery device not necessary in a high power rocket?

Page 121: Advanced  Certification Study Guide

A recovery device is always necessary

Page 122: Advanced  Certification Study Guide

A high power rocket may be constructed of what materials?

Page 123: Advanced  Certification Study Guide

Paper, wood, fiberglass, or plastic with a minimum amount of metallic parts

Page 124: Advanced  Certification Study Guide

What is a high power rocket motor?

Page 125: Advanced  Certification Study Guide

A rocket motor with more than 160 Newton-seconds of total impulse or 80 Newtons average

thrust

Page 126: Advanced  Certification Study Guide

What are the structural or load bearing parts of a high power rocket?

Page 127: Advanced  Certification Study Guide

Nose cone, body tube, and fins

Page 128: Advanced  Certification Study Guide

Who may operate a high power rocket?

Page 129: Advanced  Certification Study Guide

A person that is a certified user

Page 130: Advanced  Certification Study Guide

What operating clearances must we be in compliance with for flying high power rockets?

Page 131: Advanced  Certification Study Guide

NFPA 1127, Federal Aviation Administration Regulation Part 101 and applicable federal,

state and local regulations

Page 132: Advanced  Certification Study Guide

What criteria apply to the construction of a high power rocket?

Page 133: Advanced  Certification Study Guide

Use suitable materials to withstand operating stresses and retain structural integrity in flight

Page 134: Advanced  Certification Study Guide

When must the stability of a rocket be determined?

Page 135: Advanced  Certification Study Guide

Whenever the rocket is prepared for flight

Page 136: Advanced  Certification Study Guide

What is the maximum weight of a high power rocket?

Page 137: Advanced  Certification Study Guide

Less than the maximum weight recommended by the motor manufacturer for a given motor

Page 138: Advanced  Certification Study Guide

When is it permissible to catch a high power rocket?

Page 139: Advanced  Certification Study Guide

It is never permissible to catch a high power rocket

Page 140: Advanced  Certification Study Guide

What payloads are not permitted in a high power rocket?

Page 141: Advanced  Certification Study Guide

Payloads that are flammable or explosive or intended to cause harm AND Vertebrate

animals

Page 142: Advanced  Certification Study Guide

When must a high power rocket launching device incorporate a blast deflector?

Page 143: Advanced  Certification Study Guide

When necessary to prevent the rocket motor’s exhaust from impingng on flammable materials

Page 144: Advanced  Certification Study Guide

What is the maximum launch angle from vertical for a high power rocket?

Page 145: Advanced  Certification Study Guide

20*

Page 146: Advanced  Certification Study Guide

What are the elements of an ignition system?

Page 147: Advanced  Certification Study Guide

Remotely controlled, electrically operated, a launch switch that returns to OFF when released and a removable safety

interlock in series with the launch switch

Page 148: Advanced  Certification Study Guide

When shall the motor igniter(s) be installed in a high power rocket motor?

Page 149: Advanced  Certification Study Guide

At the launcher or designated area

Page 150: Advanced  Certification Study Guide

When shall firing circuits be armed?

Page 151: Advanced  Certification Study Guide

When the rocket is in the launching position

Page 152: Advanced  Certification Study Guide

What is the launch Site Dimensions Table used for?

Page 153: Advanced  Certification Study Guide

As the standard for minimum launch site dimensions

Page 154: Advanced  Certification Study Guide

What is the alternate launch site criteria?

Page 155: Advanced  Certification Study Guide

No less than 1500 feet AND No less than one-half the maximum altitude expected or granted

by the FAA

Page 156: Advanced  Certification Study Guide

What is the minimum distance from an occupied building or public highway for a

launch site?

Page 157: Advanced  Certification Study Guide

1500 feet

Page 158: Advanced  Certification Study Guide

How close can spectators be to a high power rocket launch?

Page 159: Advanced  Certification Study Guide

At the distance defined by, and behind, the safety monitor

Page 160: Advanced  Certification Study Guide

What is the maximum altitude allowed for flying high power rockets if there is a cloud

ceiling of 3000 feet?

Page 161: Advanced  Certification Study Guide

Neither a nor b

Page 162: Advanced  Certification Study Guide

What is the limit of surface wind for launching a high power rocket?

Page 163: Advanced  Certification Study Guide

20 mph

Page 164: Advanced  Certification Study Guide

When may a high power rocket be launched?

Page 165: Advanced  Certification Study Guide

After informing and getting permission and attention of the safety monitor

Page 166: Advanced  Certification Study Guide

High power rocket motors, motor reloading kits and pyrotechnic modules shall be stored in what

type of container?

Page 167: Advanced  Certification Study Guide

A Type 3 or Type 4 indoor/outdoor magazine AND a resealable, non-combustible container

Page 168: Advanced  Certification Study Guide

What is the minimum distance for smoking (or open flame) from high power rocket motors,

motor reloading kits and pyrotechnic modules?

Page 169: Advanced  Certification Study Guide

25 feet

Page 170: Advanced  Certification Study Guide

What quantity of high power rocket motors, motor reloading kits and pyrotechnic modules

may be stored in an indoor magazine?

Page 171: Advanced  Certification Study Guide

50 pounds

Page 172: Advanced  Certification Study Guide

According to NFPA 1127, who can produce a solid propellant high power rocket motor?

Page 173: Advanced  Certification Study Guide

A commercial manufacturer

Page 174: Advanced  Certification Study Guide

A commercial manufacturer of high power rocket motors may produce what kind of

motors?

Page 175: Advanced  Certification Study Guide

Expendable, solid propellant high power rocket motors AND Reloadable non-expendable solid

propellant high power rocket motors

Page 176: Advanced  Certification Study Guide

How much variation can there be in the certified total impulse and delay time of commercial high power rocket motors?

Page 177: Advanced  Certification Study Guide

20%

Page 178: Advanced  Certification Study Guide

When may a solid propellant high power rocket motor be shipped and stored with the igniter

installed?

Page 179: Advanced  Certification Study Guide

Never

Page 180: Advanced  Certification Study Guide

What is the key prerequisite for certification of a solid propellant high power rocket motor?

Page 181: Advanced  Certification Study Guide

Prior to classification by the U.S. Department of Transportation as a UN Division 1.3 or 1.4 explosive or written

acknowledgment of the motor or reload kit as a flammable solid

Page 182: Advanced  Certification Study Guide

When must the manufacture report changes to the authority that originally certified the

certified high power rocket motor?

Page 183: Advanced  Certification Study Guide

With in 30 days of the change

Page 184: Advanced  Certification Study Guide

Who may receive a solid propellant high power rocket motor?

Page 185: Advanced  Certification Study Guide

Certified users

Page 186: Advanced  Certification Study Guide

What is the age limit Tripoli recognizes for a certified solid propellant high power rocket

motor user?

Page 187: Advanced  Certification Study Guide

18 years of age

Page 188: Advanced  Certification Study Guide

When may a high power rocket motor be used for spectacular displays of color, light and/and

or sound?

Page 189: Advanced  Certification Study Guide

They may not be used for this application

Page 190: Advanced  Certification Study Guide

When is the sale, offering for sale and/or exposing for sale of uncertified motors

permissable?

Page 191: Advanced  Certification Study Guide

It is never permitted

Page 192: Advanced  Certification Study Guide

When is conveying a high power rocket motor to an uncertified person permitted?

Page 193: Advanced  Certification Study Guide

When the person is preparing to certify as a high power user

Page 194: Advanced  Certification Study Guide

When is it permissible to consume alcohol when prepping or launching high power

rockets?

Page 195: Advanced  Certification Study Guide

It is never permitted

Page 196: Advanced  Certification Study Guide

What organizations may certify high power rocket motors?

Page 197: Advanced  Certification Study Guide

Tripoli and NAR

Page 198: Advanced  Certification Study Guide

What organization my certify users of high power rocket motors?

Page 199: Advanced  Certification Study Guide

Tripoli and NAR

Page 200: Advanced  Certification Study Guide

What document has been adopted be the Tripoli Rocketry Association as the Tripoli Safety

Code?

Page 201: Advanced  Certification Study Guide

NFPA 1127