SPACE SYSTEMS, INC -
A Division of the AA Institute
* * * ROCKETRY & AEROSPACE PROGRAM NEWS
RELEASE - AUGUST 2003 * * *
Ascent 3 sets important new
milestones! Article posted: August 4th,
2003
The non-military (but scientifically "classified") launch of
Ascent 3 on Sunday from AA Institute's Northern Rocket Range (NRR) test
facility, recorded a number of important milestones:-
New altitude record: estimated at 1,000 feet
First successful post-landing recovery
First full function technology payload
Heaviest lift capability to date: 0.083kg integrated mass at launch,
delivering 15g of payload mass to 1,000 feet with flawless stability
Highest level of launch & tracking support: crew of 3 people
The mission successfully demonstrated new capabilities for
pin-point accuracy in recovery, using MicroBeacon's transducer pulsed
signals in conjunction with wide field
tracking & surveillance (WFTS) operations.
Despite these
ground-breaking achievements though, the post-apogee descent was far from
perfect. The internal thermal insulation, designed to protect the
parachute and the structural airframe of the rocket from hot ejection
gases during engine thrust phase, proved partially inadequate. The result
was a partially deployed and damaged parachute providing minimal
aerobraking and deceleration, which resulted in a steeper than expected
angle of ballistic descent and a stronger impact at "touchdown"!
The 1,000 foot drop from apogee was entirely tracked and some
in-flight images are published below.
Ascent 3 Mission Parameters
Parameter:
Ascent 3
results:
Launch
designation:
AA-Ascent-3
Launch
date/time:
1300 hrs GMT,
3rd August 2003
Launch
site:
AA Institute's
Northern Rocket Range test facility
Ground
crew:
3 - inclusive of
launch support & tracking
Integrated
vehicle mass at launch:
0.083kg ,
made up of:-
Launch vehicle=
42g
Propellant + motor=
24g
Payload module=
15g (including
12 volt battery)
Parachute + thermal insulation=
2g
Motor
class:
C-6-5, solid
fuel
Ignition
system:
Wired ignition
via 5m umbilical, powered by 4 x 1.2 volt Ni-MH
rechargeables
Onboard power
systems:
- 12 volt DC
alkaline cell for MicroBeacon payload module
- Pyrotechnic
ejection charge for separation burn &
parachute
Left: Ascent 3's "MicroBeacon"
payload module - the most sophisticated technology package yet flown
on an AAI launch vehicle - pictured during terminal descent
simulations in July 2003 [Credit: AA Institute]
Ascent
3 utilised a US Army micro-missile powered by a C6 class of solid
fuel motor to launch the MicroBeacon technology module during this
test flight. Based on results from this mission, the payload lift
performance for AA Institute's current fleet of launch vehicles can
be projected as follows:-
The above projections are modelled on a
vertical launch angle, constant drag coefficient (Cd=0.75) and zero
cross-winds, discounting all real world atmospheric effects that can
potentially cause the flight performance to alter from that
simulated in this model.
Ascent 3 mission images
Ascent 3 positioned on the launch pad in the high deserts north
of Luton!
After a brief
disappearence from view at the end of the powered flight, a
ground-based, still digital camera regained visual acquisition on
Ascent 3:
The below sequenced thumbnail images,
captured with a ground based digital camera at a resolution of 3.2
million pixels per frame, show the distant craft extending its
parachute during the recovery phase:
The "Rocketry &
Aerospace" program is an aspirational initiative of the AA Institute
of Space Science & Technology