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SSRP Campaign 1999-06


By asri - Posted on 13 March 2009

June 1999. Vehicles launched: S3N, S4N, Z22, Z23, Z24, Z25

June 1999
Trial Campaign


FLIGHT
SCHEDULE 
AND 
MATERIAL
REQUIREMENTS


SECTION
1. FLIGHT SCHEDULE

1.1 FLIGHT EXPERIMENTS

The
June 1999 trial will involve the launch of nine vehicles with various payload
configurations including both recoverable and non-recoverable types. The
launches will be conducted over a two day period from the 12th
to the 13th of June
.

Five
launches will be conducted on the night of the 12th of June and will carry
non-recoverable payload modules containing various tracking aids (ie. Flares,
strobe lights etc). These experiments will evaluate the effectiveness of
the tracking systems in obtaining both trajectory and relative velocity
data. The data will be recorded by obtaining photographic time exposures
of the vehicles in flight from a number of remote sites.

The
remaining four vehicles will be launched on the 13th of June. Two of the
vehicles will carry recoverable payload modules containing student experiments.
The third vehicle will also carry a recoverable payload module and will
contain DSTO IR-flare experiment. The fourth vehicle will test the flight
worthiness (ie. structural integrity) of a Zuni two stage separation system.
This experiment will carry an inert second stage and payload section. No
separation of the two stages will take place in this test.

 

1.2
PRELIMINARY FLIGHT SCHEDULE

The
flight schedule for the June 1999 trial is as follows:

 

 


Flight

Number

Module

Configuration

Description
of Payload

Material
Requirements and Responsibility (-Organisation-)

Z22N

No
payload

(Ballistic)

No
payload 

Zuni
motor (ASRI)

Z23N

Tube/cone
(Ballistic)

Strobe
light system

Zuni
motor (ASRI)

Payload Section (Woomera Area
School)

S3N

Flat
nose tube

(Ballistic)

Strobe
light & tracking system

Sighter
motor (ASRI)

Payload section (QUT)

S4N

Flat
plug

(Ballistic)

Flare
tail unit 

(10sec delay)

Sighter
motor (ASRI)

Nose plug (QUT) 


Fin unit (QUT)

Two flares (ASRI)

S5N

Flat
plug

(Ballistic)

Flare
tail unit 

(15sec delay)

Sighter
motor (ASRI)

Nose plug (QUT)

Fin unit (QUT) 

Two flares (ASRI)

Z24

ZPM2
(OLD)

Spring/mass
accelerometer


and tracking system

Zuni
motor (ASRI)

Aluminium Zuni plug (ASRI)

Z25

ZPM3
(NEW)

Infra-red
flare and launcher system

Zuni
motor (ASRI)

Payload (DSTO/ASRI) 

Steel cable & Copper crimp
(ASRI)

Cable cutter (ASRI)

Z26

ZPM3
(NEW)

Video
camera system, Fabric water resistance 

experiment and tracking 

system

Zuni
motor (ASRI)

Aluminium Zuni plug (ASRI)

Aluminium piston & plate
(ASRI)

Experiment frame (ASRI)

Steel cable & Copper crimp
(ASRI)


Cable cutter (ASRI)

Z27

Inert
payload

module and second stage

Two
stage 

Zuni with inert second stage.

Separation mechanism and inert
payload module

Zuni
motor (ASRI)

Zuni motor with inert propellant
(University of Newcastle)

Inert payload section (University
of Newcastle)

Separation mechanism (University
of Newcastle)


 

SECTION
2. MATERIAL REQUIREMENTS

2.1
ORGANISATIONAL RESPONSIBILITIES

The
organisations and individuals preparing experiments for this trial are
responsible for all material and construction costs for their payloads.
ASRI will provide technical assistance for interfacing experiments to the
recoverable payload modules.

To
prepare the recoverable payload modules for flight approximately 400mm
of 140 mm diameter Aluminium alloy bar will be required. In addition, approximately
$150.00 will be required to purchase various miscellaneous items such as
steel cable, bolts, copper crimps, electrical wire and for any last minute
machining operations required to prepare the payload modules for flight.

It
is vitally important that all the payloads be prepared and delivered to
ASRI for inspection and integration by the 30th of April 1999. Payloads
delivered after this date will not fly in the June 99 trial campaign.