Perth Advanced Rocketry Club Range Operations Manual
©1998, Perth Advanced Rocketry Club, Perth Western
Australia This document may be duplicated or modified, providing this copyright
message is retained, freely; but may not be charged for, except to
recoup copying fees. Under no circumstances may this document be
reproduced for profit, except with the express written consent of
P.A.R.C.
CONTENTS
- Definitions and Abbreviations
- Scope and Audience
- General
- Equipment
- Personnel
- Personnel Duties and Responsibilities
- RSO
- LCO
- FO
- SCO
- Trackers
- Recovery Team
- Site Preparation
- Access Permission
- Altitude Waiver
- Fire Precautions
- Range Setup
- Range Head / Launch Pad Placement
- Range Control Area
- Preparation/Loading Area
- Recovery Area
- Tracking Stations
- Spectators
Site Operations
- Acceptable Conditions
- Wind Speed
- Cloud Cover/Ceiling
- Visibility Range
- Pre-launch Rocket Safety Check
- Proof of Current Membership
- Structural Integrity
- Approved Motor
- Stability
- Recovery
- Estimated Apogee
- Special Types and Requirements
- Range Operation
- Loading Launch Pad
- Pre-launch Checks
- Tower Notification Not Required
- Tower Notification Required
- Countdown
- Tracking
- Recovery
- Holds and Aborts
Site Closure
- Tower Notification
- Equipment Recovery
- Waste Disposal
- Security
APPENDICES
- Site Permission Form
- Altitude Waiver Request Form
- Ideal Site Layout Diagrams
- RSO Range Checklist
- LCO Checklist
- SCO Checklist
- Minimum Site Dimensions Table
- Minimum Safe Distances Table
REFERENCES AND FURTHER READING
Definitions and Abbreviations
The definitions given in this section are for practical
guide purposes. In some cases strict accuracy has been
compromised in favour of clarity and brevity.
Scope and Audience
This document covers the preparations and operations
procedures for a Model Rocket or High Power Model Rocket
Range. It does not cover competition procedures, or
other similar matters.
This manual has been written for Western Australian
conditions, and it is envisaged that it will serve as
a guide for the writing of manuals designed for other
states.
At the time of writing, laws governing the use
of model rockets vary widely from state to state.
Before utilizing this manual outside of Western
Australia, you must confirm its suitability with
the local authorities, and make such amendments as
are required.
The target audience is Club officials and members intending
to use or prepare a Range.
The terms Model Rocket Engine and Model Rocket Motor
are used interchangeably throughout this document.
General
- Certification
- Qualification to use and fly model rockets of a
given power and size. Certification levels
are determined by the A.R.A. or equivalent
organizations.
- Static Stability
- The measure of the degree to which
an object is held in equilibrium,
at rest, when acted on by outside
forces. Typically measured by the
relationship between the Centre
of Pressure and the Centre of Mass
measured in units of object diameter.
Static stability is used in model
rocketry for most stability
calculations.
- Centre of Mass
- The point at which the object will balance.
- Centre of Pressure
- The point at which forces acting on the
cross-section of the object balance.
- Hold
- A pause in a countdown.
- Abort
- A cancellation of a launch.
- Apogee
- A maximum height above the earth.
- Newton-Second
- A force of one Newton applied for one
Second. (NS)
- Motor Class or Power Class
- A means of identifying the general
power level of a model rocket engine.
The basic model rocket engine is
defined to be Class A - with a total
maximum impulse of 2.5NS. Each higher
class (B,C,D,etc) doubles the maximum
power of the engine, whilst each lower
class (1/2A,1/4A) halves it.
- Impulse
- The total energy provided by a motor,
measured in Newton-Seconds.
- Motor Type
- A specific engine variety, specified
in terms of Class, Average Thrust and
Delay Time after burn-out.
- Newton
- The force required to accelerate 1kg
by 1m/s/s. (N)
- CASA
-
- The Civil Aviation Safety Authority.
- Airservices
- Airservices Australia.
- Waiver
- A document detailing an exception to
a regulation; usually referring to a
permit to use airspace to a given
altitude.
- Ceiling
- The maximum height permitted.
- Visible Range
- The maximum distance at which object
can be seen by the naked eye.
- AGL
- Above Ground Level.
- ASL
- Above Sea Level.
- Cloudbase
- The minimum altitude occupied by clouds.
- Controlled Airspace
- Any airspace above 300' AGL
- LWR
- Lift to Weight ratio; the ratio between
the initial thrust of a motor and the
mass of the model.
- Member
- A current financial member of the Perth
Advanced Rocketry Club, the Australian
Rocketry Association, or organization
affiliated with the Australian Rocketry
Association.
Equipment
- Launch Pad
- A device designed to hold a rocket in
an upright position prior to flight.
- Launch Controller
- An electronic device used to
control the ignition of model
rocket motor.
- Model Rocket
- A device propelled by a self-contained
reaction device that is commercially prepared
and recovers in a safe and controlled manner.
Model rockets may use motors up to class D,
and mass no more than 500g. Model rockets
are non-metallic or contain minimal
metallic parts in non-structural roles.
- Large Model Rocket
- A model rocket that masses up to 1500g, and
uses any motor with a propellant mass less
than 62.5g. To date, this limits the power
class to G.
- High Power Model Rocket
- A model rocket, that masses over 1500g and
uses motors with more than 62.5g of propellant.
Upper power class is O.
- Model Rocket Motor
- A pre-built or pre-fabricated self-contained
reaction device. Pre-fabricated types
must be used as directed by the manufacturer,
without modification.
- Approved Model Rocket Engine
- A model rocket motor that has been
approved for use by a suitably
qualified body. Example bodies
are:
- Australian Rocketry Association
- National Association of Rocketry
(U.S.A.)
- Tripolli Rocketry Association
(U.S.A.)
- Recovery Device
- Any means of returning a model rocket
to the ground in a safe and undamaged
state.
- Safety Interlock
- A removeable device required for
a launch controller to become active.
- Igniter
- An electrically operated device that
ignites a model rocket engine.
- Payload
- An object carried by a model rocket
that does not have a structural or
aerodynamic purpose.
- Airframe
- The non-engine, non-payload portions of
a model rocket.
- Wadding
- Flame-proof material used to protect a
recovery device from a motor's ejection
charge.
- Boost Glider
- A glider lifted in a ballistic manner
by a rocket that detaches from the
glider. The glider then transitions
to an aerodynamic profile, and the
booster recovers by other means.
- Rocket Glider
- A glider lifted in a ballistic manner
by a rocket that is retained. The
glider then transitions to an
aerodynamic profile, and recovers
intact.
Personnel
- RSO
- Range Safety Officer
- LCO
- Launch Control Officer (Sometimes also
called Range Control Officer)
- SCO
- Safety Check Officer
- FO
- Fire Officer
- Tracker
- Person designated to track the flight
of a model
- Recovery Team
- Person or persons designated to recover
a model after landing
- Flyer
- Person responsible for the flight of a
model
- Spectator
- Any person in the area not involved
in a) the operation of the range
b) the flying of the model
Personnel Duties and Responsibilities
This section defines the duties and responsibilities of the range
officers. For small meetings, some of these roles may be merged.
The Safety Officer roles, however, are always separate from the
other roles.
RSO
The RSO has to ensure that the range is operated safely
and legally at all times. They are not there to make
life hard for flyers, but rather to protect them from
their own enthusiasm. If they must, the can ask flyers
to leave, and the close the range if things get out of
hand. They can reject rockets as unsuitable for the range,
dangerous, or not legal to fly. They must prevent flyers
from launching outside of their certification. They CANNOT
prevent a launch because of dislikes - they must validate
all their decisions at all times. If a flyer wishes, they
may discuss the RSO's decision, but it is the RSO that
must make the final go/no-go choice. As a matter of
protocol, another RSO may not accept another's rejection,
in the event of the post being passed to another person
(eg at a shift change).
The RSO may also close the range if conditions become
unsafe, or for any other reason. The RSO also has the
power to assign duties to others on the range, and to
relieve range officers of their duties if they are not
performing them adequately.
LCO
The LCO's role is to ensure that the pad area is run
safely, and quickly. They are to assist in speeding
the turn-over of rockets on the pads, and are there to
help flyers see as many *safe* launches as possible.
The LCO has control over which pads are in use, the
launching order, what models are allocated to which pads,
and announce each launch. They may also issue countdowns
for flyers.
FO
An FO, if needed, watches the pad area for signs of fire
resulting from a launch. He MUST watch the pad area at all
times, and not watch flights at all. As for other safety
positions, this should be rotated. An FO is not needed if
launching from short green grass, sand, or other
non-flammable surface.
SCO
An SCO is responsible for checking models that are to be
presented to the LCO for launch. They must ensure that the
model is sound and safe to fly, and that the fitted motor(s)
and recovery device(s) are correct and appropriate. If an
SCO is unsure of the safety of a model, he may choose to
either reject it (giving the reasons, and how they may
be addressed), or request a ruling from the RSO.
Trackers
Trackers are responsible for keeping the model in view
during flight. They may also have additional duties,
such as measuring altitude.
Recovery Team
A Recovery Team is responsible for retrieving a model
once it has landed. This role is often filled by the
flyer.
Site Preparation
This section deals with the procedures to gain access to a site,
arranging appropriate altitude clearances, and the physical set-up
of a range.
Access Permission
Before any activities can be begun, written permission for
the use of the selected site must be obtained from the
owner or manager of the site. A suitable form is given in
appendix A.
Ceiling
Every site has a ceiling; this ceiling is the minimum
of:
- 300'AGL or the issued waiver
- Four (4) times the minimum dimension of the site
- The current cloud-base
Altitude Waiver
If flight operations are going to exceed 300'AGL,
then an appropriate waiver or permission must be
sought from the Civil Aviation Safety Authority.
Sites intended for regular or frequent use may
be issued (on application to C.A.S.A.) with permanent
permission for a given ceiling. If that altitude is
intended to be exceeded, or the site is intended for
occasional or infrequent use, then a specific waiver
must be obtained. A suitable form for requesting a
specific waiver is given in appendix B.
Specific waivers have a lead-time of 14 days.
Fire Precautions
No flight operations are permitted during a posted
Total Fire Ban, or during a period of posted Very
High or Extreme Fire Danger in the site's region.
In areas where grass fires are a possibility, a
non-flammable tarpaulin or blanket should be placed
under each pad, and extend at least 1/10 of the
minimum safe distance around the pad.
Range Setup
The boundaries of the range should be clearly marked,
and, if possible, the individual areas of the range
also marked.
Range Head / Launch Pad Placement
The range head and launch pad area should be placed
as near as is practical to the centre of the range
area. If there is a prevailing breeze, this area
maybe offset up to 1/4 of the site dimensions upwind
of centre, so as to provide more recovery area.
The only personnel permitted in this area are:
RSO, LCO and Flyers. The only exception is
when a person is given specific and explicit
permission by the RSO.
- Pad Separation
Launch pad are to be separated by the
minimum safe distance for the rockets
being launched from them, as given in
the appropriate safety code. The
exception to this is for launch racks,
where a number of rockets are prepared
simultaneously and launched sequentially.
Such racks should be treated as one pad
for safety purposes.
- Pad Specifications
All launch pads are rated for models of
certain sizes.
A launch pad must:
- Be capable of supporting the largest
model it is rated for.
- Have a rigid guide for the model to
travel along prior to gaining flight
speed. A guide must be designed such
that it prevents the model from leaving
the guide until it has travelled the
entire length of the guide.
- Either be unable to be tilted past
30 degrees from vertical, or be
clearly marked as to when that angle
is exceeded.
- Have a means of protecting the ground
from the exhaust of the rocket.
- Be stable when loaded.
Range Control Area
The Range Control area should be immediately
North of the pad area, and is where the launch
controllers are placed. This is also the area
that the LCO operates from.
All controllers must be clearly linked to the
appropriate pad.
Non-flying personnel may not enter this area
without the permission of the LCO or RSO.
Preparation/Loading Area
The Preparation/Loading Area is North of the
Range Control Area. This area is open to the
public, and is where models are prepared for
flight. SCO inspections are also carried out
in this area.
Recovery Area
The Recovery area is all areas not otherwise
specified. Most (and ideally all) recoveries,
however, will take place in the area South
of the Range Head. This area is also termed
"Down-range".
Tracking Stations
If measured tracking is taking place (ie
theodolite tracking for altitude determination)
then the tracking stations should be placed
as far North on the range as possible, and
placed in opposite corners of the range
to the East and West.
Spectators
The spectator area is to the North of the
Preparation Area, and may include a parking
area.
Site Operations
This section relates the operation of an active range. Also
refer to the RSO Range Checklist (appendix D).
It is acceptable practice for RSO, SCO, FO and LCO duties to be
combined, and for the Flyer to assume the duties of tracking
and recovery. Thus the minimum personnel for a range is two.
Acceptable Conditions
In addition to the conditions addressed in this section,
a "safety first" attitude must be observed. Any unexpected
conditions that could affect spectators, other air users,
or the area surrounding the range should also be considered.
Wind Speed
During launching, the wind-speed must not
exceed the maximum specified in the P.A.R.C.
safety code applicable to the rocket being launched.
If possible, a simulation should be run to
ensure that the rocket being launched will
recover in the recovery area.
Cloud Cover/Ceiling
Cloud cover must not exceed 1/8 at any point
in the flightpath.
Flights into airspace containing greater than
1/8 cloud cover are prohibited, as are any
flights that will penetrate a cloud-mass. To
ensure this, the ceiling will be the lower of
the posted waived altitude or the cloudbase,
less 10% of the altitude of the cloudbase.
Visibility Range
A visibility of 6NM at all levels in the site's
airspace, up to its operating ceiling is required.
Recovery Area Obstructions
If the Recovery Area contains vehicles, animals
or people not part of a Recovery Team, the range
will be closed until the obstruction is cleared,
or has left the area.
Pre-launch Rocket Safety Check
This check is performed in the Preparation Area by
the SCO. The SCO may request a ruling from the RSO,
if they are unsure of any point. In any event, the
RSO's rulings are final.
Only current financial members may present models
for checking an launch. A current financial member
may present a third party's model, but assumes full
responsibility for that launch. This does not confer
permission for a third party to undertake the actual
launch. See also 4.3.3
Proof of Current Membership
The first time a Flyer presents a model to
be checked at any given session, they must
present their membership card, or other
proof, showing a valid financial membership.
Structural Integrity
The airframe and motor-mount will be constructed
so as to be able to withstand the stresses of
launch and recovery with the fitted motor and
recovery device.
Approved Motor
The motor being used must be:
- An approved model rocket motor
- Provide a LWR greater than 4
- Have a delay that will ensure safe recovery
Stability
The model will exhibit at least 2 calibers of
static stability, or be of an otherwise proven
design.
Design test flights may be carried out if the
range has been opened for the express purpose
of design testing.
Formal proof of design stability (using the
Barrowman centre of pressure calculations) is
an acceptable substitute for previous flights.
Recovery
The fitted recovery device must be properly
attached and packed, and be designed to recover
the model safely. Any protective wadding must
be of an approved type.
Estimated Apogee
The estimated apogee must not exceed the site
ceiling.
Special Types and Requirements
Special types of model may require additional
considerations. These include R/C gliders,
Boost-Gliders, staged models, clustered engines,
and specialized payloads. Examples of these
are given in the SCO Checklist (appendix F).
Range Operation
This section is summarized in appendix E, the LCO
checklist. Any model presented for launch must
have passed the pre-flight check.
Launch Pad Loading
During the loading process, the Flyer,
who must be present during the loading,
must retain the safety interlock for the
pad being loaded.
Only personnel required to load the model
onto the launch pad are permitted to
approach the pad during the loading
operation, unless specifically approved
by the RSO. Approval must be given in
each and every instance.
The rocket must be loaded onto a pad
that has specifications that at least
match the model's requirements.
After loading onto the pad, any other
pre-flight preparations are made (eg
removing protective hoods from lenses,
arming recovery systems).
After all other pre-flight preparations
are made, the model's ignitors are
connected to the launch controller.
After the ignitors are connected, all
personnel must leave the pad area.
Pre-launch Checks
The safety interlock is inserted into the
launch controller, continuity is confirmed
through the ignitors, and the pad is announced
as armed. If continuity is not established,
then the safety interlock is removed, and
the loading personnel may be permitted to
approach the pad to correct the problem at the
LCO's discretion. The LCO may choose to abort
the launch and require the model to be removed
for diagnosis and correction.
- Tower Notification Not Required
The LCO checks the surrounding airspace
and the recovery area, and, if clear,
gives the go-ahead for launch.
- Tower Notification Required
The LCO contacts the appropriate
ATC, as advised by CASA, and informs
them of the launch location, the
waiver reference, and intended altitude.
If a series of launches will be following,
an estimated end time must also be
provided. If the ATC gives clearance,
then the LCO proceeds as per 4.3.2.1. If
clearance is not given, then either a
hold is placed until it is given, or
the launch is aborted.
Countdown and Launch
The Flyer must be a current financial member
of the club. With specific and explicit permission
from the RSO, a flyer may designate a third party
to perform the actual act of launching. Under such
circumstances the third party must be under direct
supervision by the flyer at all times.
The LCO, or by the LCO's choice the Flyer,
will issue a five second count down, as follows:
"Five, Four, Three, Two, One, Start"
During the Countdown, the LCO will maintain
a lookout for hazards, and may call a hold
at any point.
At the call of "Start", the launch controller
will be activated by the flyer.
If the engine(s) fail to ignite after two (2)
seconds, the flyer may request a re-count, or
safe the controller.
After safing, the LCO may permit (after no less
than 60 seconds) the flyer to attempt to correct
the ignition problem at the pad, or order an abort.
Tracking
The model will be tracked, as far as is practical,
through its flight, to the point of landing, by
at least one person.
Tracking may be interrupted by the LOS being blocked,
or by the model traveling too fast to track, or by
being too small to track at its apogee. If at all
possible, the track should be regained as soon as
is possible.
Failure to successfully track may result in
the model being unrecoverable.
Recovery
Once the model lands, is position should be noted by
the recovery team, who then approach the model,
safe any payload, and return it to the flyer.
Holds and Aborts
Holds may be called by any person spotting a
hazard during a countdown. After a hold, the
LCO determines the nature of the hazard, and
either restarts the countdown (from the start)
calls an abort, or requests clarification from
the RSO.
Aborts may be called by the RSO, the LCO or
the flyer. After an abort the controller
is safed, and the model removed from the pad.
Once the cause of the abort has been resolved,
the model may be re-presented for launch.
Site Closure
These procedures are to be followed after the range has been
closed, and will not be re-opened that day.
Tower Notification
If flights have required local Air Traffic Controllers
to be notified, they are to be informed that the ranged
is now closed and will not be re-opened that day.
Equipment Recovery
All ground equipment is to be safed, checked for damage
by the RSO, and packed. If equipment belongs to specific
persons, it is to be returned, and club equipment passed
to the responsible officer.
Waste Disposal
After all equipment has been packed, the site is to be
searched for launch debris (eg used wadding, ignitors, etc)
and other rubbish.
Particular attention is to be paid to the pad areas,
where there may be numerous small items remaining.
Security
After all other personnel have left, the site is to
be secured by the RSO and the LCO, jointly. The level
of security required is to be determined by the site
owners/managers.
APPENDICES
Site Permission Form
Site Approval for the Launch of Model Rockets
I, __________________, being the owner/occupier of the property listed
below, or the owner's/occupier's delegated authority, give permission
for model rockets to be launched to an altitude of ______ feet AGL,
on ____/_____/____ from the hours of ___:___ to ___:___.
This permission is subject to the following restrictions:
A/ Site Fees (indicate those that apply):
( ) Each person launching will be required to pay a fee of $___.___
per day.
( ) The club/group launching will be required to pay a fee of $___.__
per day.
( ) No fee will be levied.
B/ Altitude Waiver
Should the permission extend to altitudes in excess of 300 feet AGL,
a valid waiver from the Civil Aviation Safety Authority must be
held, and the conditions of that waiver followed.
C/ Fire Hazards
No launch shall be permitted in a total fire ban.
( ) Fire extinguishers required.
If required they must be of an appropriate approved type.
D/ Other Conditions
______________________________________________________________________
______________________________________________________________________
______________________________________________________________________
______________________________________________________________________
______________________________________________________________________
Signed,
_________________________________ (Name)
_________________________________ (Position)
Property Details:
______________________________________________________________________
______________________________________________________________________
______________________________________________________________________
______________________________________________________________________
______________________________________________________________________
Altitude Waiver Request Form
___________________
___________________
___________________
___________________
___________________
Ph: (h) (08) _________
(w) (08) _________
FAX: (08) _________
___ ________________________
Flying Operations Inspector
CASA
Perth District Office
PO Box 1082
Cloverdale
6985
Ph : 131757
FAX: 08 9366 2891
_________________, ______
APPLICATION FOR APPROVAL UNDER CIVIL AVIATION REGULATION 295
TO LAUNCH ROCKETS
Dear ___ ________________,
I/we are seeking permission under CAR 295 to launch model rockets over
100 metres. I/we have listed the relevant details:
(1) A weight restriction of 1000/______ grams will apply.
(2) The maximum height above ground level of flights will be _____ feet.
(3) The estimated safety buffer above maximum height of flights will
be _____ feet.
(4) The maximum horizontal distance of flights will be ______ metres.
(5) The location is _______________________________________________.
Please refer to the attached map for the exact location of the
operation. We have/do not have written permission of the landowner/
occupier to conduct this launch.
(6) Dates of flying are _____________________. The duration of these
operations will be from ____hrs to ____hrs local time. I/we may be
contacted during these times on _________________.
(7) The event will be overseen by _____________ as Range Safety
Officer, under the codes of the Australian Rocketry Association
and according to the Range Operations Manual of the Perth Advanced
Rocketry Club.
Sincerely,
______________,
Perth Advanced Rocketry Club member#____-__.
Ideal Site Layout Diagrams
RSO Range Checklist
Range Situation
1. Is range large enough for ceiling?
2. Is pad area clear?
3. Is spectator area at appropriate distance behind firing line?
4. Are prep areas, firing line, spectator line all clearly marked?
Range Closure Conditions
1. Is cloud below waiver ceiling? (Reduced ceiling is an option.)
2. Is wind above maximum safe speed?
3. Limited visibility?
4. Airspace occupied?
5. ANY OTHER CONDITION THAT THE RSO FEELS WARRANTS THE CLOSING OF THE
RANGE.
RSO POWERS
1. A rocket may be rejected for any reason.
2. A flyer may be asked to leave the range for any reason.
3. A countdown may be halted for any reason.
4. A range may be closed for any reason.
5. Any flyer attempting to bypass the RSO or any other officer
of the range *will* be ejected for compromising range safety.
An RSO *MUST* justify their rejection, closure or ejection
from the field.
LCO Checklist
Setup
1. Ensure all pads/controllers are at at least minimum safe distance.
2. Number each pad and controller clearly.
3. If possible, separate
Pads Empty
1. Are all controllers clear?
2. Call for flyers.
3. Check each flyer has cleared the SCO
4. Allocate 1 flyer per pad.
5. Mark flyer, motor, and model on flight sheet.
Pre-launch
1. Pad area clear?
2. Recovery area clear?
Loaded Pads
1. Call flyer name, model and motor.
2. Check airspace for other users.
3. Call " clear to launch!". If misfire, call
"Hold !".
4. Repeat for each pad.
If any misfired pads remain at end of sequence, allow re-try,
then remove from pad to diagnose.
In the case of drag-race launches, announce all all fliers and
pads as a group.
SCO Checklist
General:
1 / Is flyer a valid member?
2 / Is the motor approved?
3 / Does the flyer have the appropriate certification for
the motor in use?
4 / Motor properly retained?
5 / Is the delay correct?
6 / Is the LWR>4 (ie enough thrust to lift the model safely)?
7 / Is the model aerodynamically stable?
8 / Is the model structurally fit to fly with the fitted motor?
9 / Are the ignitors suitable for the motor?
10/ Is the recovery device securely fitted, and correctly packed?
11/ Is the nosecone/payload bay correctly fitted (too loose too snug?)?
12/ Are any launch lugs strong enough, and securely fitted?
13/ Is the proposed altitude in excess of the ceiling?
Radio Control Only
1/ Flyer has Frequency Control Pin?
2/ Legal frequency?
3/ Can system be disarmed until ready to launch?
Ejection Controlling Altimeter Only
1/ Can the system be disarmed until ready to launch?
2/ Properly wired?
3/ Can the altimeter be activated with the ejection
leads isolated?
4/ Power supply fresh and secure?
5/ Proper indicators from altimeter module?
6/ Compartment properly vented?
7/ Compartment isolated from ejection charges?
8/ (dual deployment systems only) Main system secure enough
not to deploy on drogue deployment or apogee?
Multistage Only
1/ Each stage combination stable?
2/ Each stage has appropriate recovery system?
3/ If separating by drag, do the stages separate easily?
4/ Is the upper stage delay appropriate?
Flight Recording Sheet
+----+---------------+-----------------------+---------------------------------+
| | DATE: |FIELD: |LCO: |
+----+---------------+-------+---------------+-------+-------+----+-------+----+
|Time|Flyer Name |Mem# |Model |Mass |Engine |SCO |Est Alt|Rec?|
+====+===============+=======+===============+=======+=======+====+=======+====+
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| | | | | | | | | |
| | | | | | | | | |
| | | | | | | | | |
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+----+---------------+-------+---------------+-------+-------+----+-------+----+
Minimum Site Dimensions Table
Installed Total Impulse (NS) |
Equivalent Motor Type |
Minimum Diameter (Metres) |
0.00-1.25 |
1/4A-1/2A |
15 |
1.26-2.50 |
A |
30 |
2.51-5.00 |
B |
60 |
5.01-10.00 |
C |
120 |
10.01-20.00 |
D |
150 |
20.01-40.00 |
E |
300 |
40.01-80.00 |
F |
300 |
80.01-160.00 |
G |
300 |
160.01-320.00 |
H |
460 |
Minimum Safe Distances Table
Installed Total Impulse (NS) |
Equivalent Motor Type |
Minimum Distance(Metres) |
0.00-1.25 |
1/4A-1/2A |
5 |
1.26-2.50 |
A |
5 |
2.51-5.00 |
B |
5 |
5.01-10.00 |
C |
5 |
10.01-20.00 |
D |
5 |
20.01-40.00 |
E |
9 |
40.01-80.00 |
F |
9 |
80.01-160.00 |
G |
9 |
160.01-320.00 |
H(As 2xG ONLY) |
9 |
REFERENCES, FURTHER READING, AND SOFTWARE
Handbook of Model Rocketry, 6th Ed; Stine, G. Harry; John Wiley & Sons;
ISBN 0-471-59361-3.
Australian Rocketry Association "Blue Book"; Australian Rocketry Association. (PO Box 777 Marleston S.A. 5033)
Newsgroup posting to rec.models.rockets, 17th May 1997, by
"rocketweb@aol.com" (Douglas Caskey) based on work by John Ritz.
Perth Advanced Rocketry Club Safety Codes.
The rec.models.rockets newsgroup.
The rec.models.rockets FAQ. Available from the rec.models.rockets archive
at http://sunsite.unc.edu/pub/archive/rec.models.rockets/RMRFAQ/.
The 2d (Alt + Time) simulation program RASP, by Kent Hoult, et al.
Available from the rec.models.rockets archive
at http://sunsite.unc.edu/pub/archive/rec.models.rockets/RASP/.
The 3d (Alt, Drift + Time) simulation program RSIM, by Kenneth S. Hutchinson.
Available from the rec.models.rockets archive
at http://sunsite.unc.edu/pub/archive/rec.models.rockets/PROGRAMS4/rsim13.zip.
The stability calculation program VCP, available from Impulse Aerospace at
http://www.impulseaero.com/Software/VCP/index.html.