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Propulsion: Safety, Handling, and Test Procedures By Mac Seidel
18

Introduction to Propulsion: Rocket Engines

Feb 26, 2022

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Page 1: Introduction to Propulsion: Rocket Engines

Propulsion:Safety, Handling, and Test Procedures

By Mac Seidel

Page 2: Introduction to Propulsion: Rocket Engines

General Propellant Safety*Evaluate Safety and Handling Before

Finalizing Propellant Selection

Some Considerations• Toxicity

• harmful to the environment or human

health when coming in contact

• Exothermal Decomposition• rapid reactions can be dangerous by

releasing lots of heat

• Explosive• decomposes or rearranges with extreme

rapidity, yielding much gas and heat

• Volatility• how readily a substance vaporizes

• Flammability• ability to ignite and combust

• Cryogenic• boiling points below -150°C

• Hypergolic• fuels that ignite spontaneously upon

contact

Hyperbolic Fuels

Hazard Symbol Ex.

Page 3: Introduction to Propulsion: Rocket Engines

Nitrous Oxide Properties• Non-cryogenic, liquid oxidizer

• Density and vapor pressure are highly

dependent on temperature

• Colorless, odorless

• Can displace air and cause asphyxiation

• Can get cold and cause frostbite

• Possibility of rapid exothermic

decomposition

• Avoid direct contact with skin

• Open cylinder valve slowly

• Thermodynamic Properties of N2O• Tables of properties for range of

temperatures

• Chemical Properties and Hazards• Data sheet from PRAXAIR

• Instructions for danger relief

Linde N2O Vapor Pressure

N2O Density

Page 4: Introduction to Propulsion: Rocket Engines

Nitrous Material CompatibilityIncompatible• Organic compounds

• Materials not rated for oxygen use

• Copper, nickel, other catalysts

• Viton, FKM, FPM are chemical compatible but

are swelling significantly when exposed to

N2O (spl.ch)

• Certain grades of elastomers such as Viton®

or Neoprene® are known to swell (AGIA)

Compatible• 304 and 316 Stainless Steel, Aluminum, PTFE

and other Teflon's, Kalrez/FFKM

• PTFE, PCTFE, FEP, PEEKTM, and EPDM

(AGIA)

Elastomer O-rings

Stainless Steels

Page 5: Introduction to Propulsion: Rocket Engines

Nitrous Pros/ConsPros

• Decent availability

• Nontoxic

• Relatively “safe”, only if handled with

caution and safe practices by knowledgeable

personnel

• Easy storage in cylinders

Cons

• Density (therefore performance) highly

dependent on temperature

• Need to have high system pressures to

stay above vapor pressure

• Greenhouse gas

• Susceptible to two phase flows

Two Phase Flow Regimes

Common for Performance Cars

Page 6: Introduction to Propulsion: Rocket Engines

Nitrous Dangers• Decomposition can occur at elevated temperatures

or in contact with incompatible materials

• Explosions have occurred• Industrial and rocketry projects

• Sources like contaminations, local heating,

adiabatic compression/water hammer,

combustion instabilities, electrostatic discharge,

reverse flow of hot chamber gas into tank vapors

• Freezing of valves and/or vents• Temperature decreases with venting

• Good solubility in oil, grease, plastics, and other

hydrocarbons• Creates highly explosive material

• Be very carful of seals, Viton has been used, if

swelling is observed then try Kalrez

(FFKM/FFPM)

• Asphyxiation from vapors

• More on dangers and suggestions• SPL, Is nitrous oxide safe?

• Air Force, Nitrous Oxide Explosive Hazards

• Aspirespace, Hybrid Safety

• More in google drive Scaled Composites

Hybrid Motor

Linde N2O Storage Facility

Page 7: Introduction to Propulsion: Rocket Engines

Nitrous Safety and HandlingRecommendations

• Be extremely attentive when ox cleaning lines

• Use nitrous and pressurant filters • 500 to 150 micron for gases (AIGA)

• Max pressurizing rate of 20 psi/s (SpaceDev)

• Keep nitrous temperatures low

• Electrically ground tanks

• Remote testing operations

• Decent injector pressure drop to avoid

combustion instabilities

• Never run cold flows with nitrous• Use water or CO2

• Avoid nitrous vapors going through engine

• Avoid two phase flow by further pressurizing

with inert gas• N2 or He

• Note that N2 is soluble in N2O, but should be

fine if pressurizing for short periods

• AIGA Safe Practices for N2O• Additional Info

AIGA Oxidizer Pipe Velocity

Page 8: Introduction to Propulsion: Rocket Engines

Vapor Lock and Temperature Effects on Filling• Vapor lock

• When the flow of liquids stops due to

vaporization of the liquid

• Flow is driven by pressure differential

• NO2 Filling• Sometimes use a pump, but not always

needed

• As vapor in NO2 tanks build, the pressure

differential decreases

• To keep pressure difference use small tank

vent, or maintain temperature differential • Temperature drives NO2 vapor pressure

• Can use ice around run tank and cool

down by venting

• Could use warm water over fill tank, not

hot though

NOS Fill Station Ex.

Page 9: Introduction to Propulsion: Rocket Engines

Ethanol Safety and HandlingProperties and Hazards• Different concentrations available

• Lower concentrations with water yield lower

combustion temperatures

• Highly flammable

• Avoid direct contact with skin

• Low volatility but vapors still present, don’t inhale

• Data Sheet

Incompatible Materials (degradation over time)• brass, lead, zinc and lead-based solder

• natural rubber, polyurethane, cork gasket material,

leather, polyvinyl chloride (PVC) polyamides, and

certain thermoplastic or thermoset polymers

Compatible Materials (resistance to degradation)• unplated steel, nickel-plated steel, stainless steel,

black iron and bronze

• reinforced fiberglass, Buna-N, Neoprene rubber,

polypropylene, nitrile rubber, Viton and Teflon

Ethanol Material Compatibility

Chart (google doc)

Page 10: Introduction to Propulsion: Rocket Engines

Personal Protective Equipment (PPE)When to use?

• Leak testing

• Pressure testing

• Hot fires

• Manufacturing

• Anytime when handling hazardous

chemicals, pressurized systems, or

dangerous equipment

• Check for proper PPE before testing!

Typical PPE

• Safety goggles

• Face shield

• Nitrile gloves

• Ear plugs

• Long pants

• Closed toe shoesVarious PPE

Page 11: Introduction to Propulsion: Rocket Engines

Oxidizer Cleaning• Oxygen rich environments need to be clean

of dirt, rust, organics, etc.• If not, then there’s a large fire hazard

• Use different solvent chemicals for

different materials or situations

• Ex: isopropyl alcohol, acetone,

trichloroethylene, simple green

• Basic Procedures• Pre-cleaning

• Deep cleaning

• Rinse in DI water

• Dry with nitrogen gas or in lab

convection oven

• Inspect visually with UV light and lint-

free wipes

• Bag in plastic zip-locks and label

• Standards• ASTM G93

• NASA Safety Standards for Oxygen

• Other team’s procedures

• Specifically for Nitrous Oxide• SpaceDev Report

• Youngblood Paper

Ultrasonic Cleaner

Lint-free Wipes

Page 12: Introduction to Propulsion: Rocket Engines

Pressure and Leak TestingLeak Testing• Ensure leak tight connections before using

propellants

Pressure Testing• Proof test tanks, engines, or other plumbing for

pressurized use

• Typically to 1.2-1.5 FOS, different standards and

requirements out there, so check before doing

• Pneumatic pressurization• Inert gas like nitrogen or helium, helium

molecules are small so it is very good at

finding cracks

• Compressible, so there can be danger of rapid

expansion of gases throwing loose fittings,

hoses, or fragmentation

• Depending on pressure range, can test in

person or far away by monitoring sensors

• Hydrostatic pressurization• Need hydrostatic pump and water

• Less hazardous since lower expansion

potential, incompressible

• At high pressures, possibility of water jet

cutting hazardHydrostatic Pumps

Hose Whip Arrestors

Page 13: Introduction to Propulsion: Rocket Engines

Pneumatic Leak Testing Procedures• Not bad idea to do hydrostatic proof test first

• Could also do hybrid test with nitrogen pressing on

water

• Connect nitrogen cylinder with pressure regulator to

pressurize system• Set regulator pressure before allowing gas to

flow through rest of plumbing

• Check each fitting by applying drops of leak detection

fluid, like Snoop (soapy water)

• Pressurize section, check fittings/monitor decaying

pressures, depressurize, tighten fittings where

needed, and repeat• Slowly go up to about 110% of nominal system

pressures, (not above MAWP)

• Use increments of 50-100 psi

• Only increase pressures when no leaks are

detected

• Never adjust fittings while pressurized

• Progressively test feed system in smaller sections to

isolate leaks

• Can torque stripe fittings after all leaks fixed

• This allows to keep track of fittings already

tested and easily show if any become un-

torqued

Snoop Bottle

Torque Stripping

Bubbles Indicate Leak

Page 14: Introduction to Propulsion: Rocket Engines

Cold Flows and Ignition TimingCold Flow Testing• Flow fluids through feed system and injector

without combustion• Use safe fluids with similar properties, like

water or CO2

• For calibrating system and evaluating

performance• Determining pressure drops, flow rates, flow

coefficients, injector atomization, any issues,

etc.

• Determine actual set pressure of regulators,

can use needle valves in place of engine to

simulate pressure drop

• Determine Cv or Cd coefficients for injector,

make sure to use desired pressure drop

Ignition Timing• Test timing of ignitor in relation to propellant flow

• Good ignition timing is needed to ensure

propellant ignition and avoid hard starts • Light ignitor before opening propellant valves

Fluid Impulse

Purdue Pintle Injector

BURPG Impinging Injector

Page 15: Introduction to Propulsion: Rocket Engines

Developing Testing Procedures• Plan out operating and contingency procedures in clear

lists to read off during test day• SOP – instructions to carry out testing operations

• COP – instructions to follow in case of off nominal

conditions, if stuff goes wrong

• Walk through step by step, and write down line by line

specific, concise operation instructions• Think through each step and what states each part

of the system will be in

• Safety should be most important priority

• Include the action, the component name, target values,

and expected results

• Make sure to include verification checks of valve

positioning, data collection, power supply, etc.

• Revisit and revise procedures many times to catch

errors and constantly improve• Make sure to keep track of edits and reasoning

• Practice running them in person without propellants to

nail down all steps and ingrain into memory• Make sure all test technicians and control operators

know these

• Get them reviewed by a professional if possible

Draft of NETS Operating Procedures

Page 16: Introduction to Propulsion: Rocket Engines

Risk and Hazard Analysis• Create a document or chart of the potential

hazards that could occur and how to mitigate them• Ex. Leaking propellant, ignition failure, etc.

• Could include danger level, likelihood,

preventative measures, possible causes, etc.

• MASA has a good example in their Spaceport

doc

• HAZOP – Hazard and Operability Study• Go through each plumbing component and

operating process

• Determine what the expected result would be if

each part fails

• If it poses a serious hazard then try to find a

design solution to fix it

• Very tedious but can easily help to find flaws Rocket Engine Diagram

Basic Hazard Analysis

Page 17: Introduction to Propulsion: Rocket Engines

TNT Equivalence and Safe Testing Distance• TNT Equivalence is a common measure of energy released

from an explosion• It compares the energy in a system to the energy per

weight of TNT• TNT Energy = 4850 kJ/kg

• Different models/equations for calculating stored gas

energy release, isentropic model is historically common

• Include all compressed gas cylinders, in case of rupture

• Include decomposition energy of nitrous present

• Safe Stand-off Distances• The TNT equivalence can then be used to determine safe

distances for testing

• Different for enclosed or open space, can lessen affected

area by enclosing test or using shielding

• Distances vary for dangers• Blast wave vs. Fragment throw

• Overpressure: Glass break (0.2 psig), Ear drum rupture

(2.4 psig), Lung hemorrhage (14.5 psig)

• Some Resources• DOE Stored Energy Risk Analysis

• Understanding Explosives• See Appendix B

• ASME Pneumatic Testing Distances• Safe distances for TNT weights

• ASME PCC-2 Mandatory Appendix 501-II, pg. 253-255

• Piping-World online summary

Compressed Gas Energy Release

(Isentropic Method)

Nitrous Decomposition

TNT Equivalent

Weight

Scaled Blast Radius

Page 18: Introduction to Propulsion: Rocket Engines

Additional Resources• Google Drive: Nitrous Safety and Handling Folder

• Doc with lists of safety and handling info and links to helpful sources!!!

• Material compatibility pdf’s

• Ox line cleaning and safety

• TNT equivalence calculations

• Aspirespace• Hybrid Safety

• Has info on nitrous as well as other oxidizers

• Purdue Video• Safety Procedures and Best Practices

• Mach 5 Low-Down • Rocket Test Stand and Testing Tips

• Gas Cylinders• Penn State Policies

***Please feel free to add information/slides for future presentations!!!