Successful
Flight Test of the Prospector 6 NLV Development Vehicle
May 24, 2005
The successful launch
and recovery of the Prospector 6 (P6) test vehicle on Saturday,
21 May 2005 represents another important milestone for the joint
industry / academic team that is working to develop a low-cost
Nanosat Launch Vehicle (NLV) that will be dedicated to delivering
10 kg payloads to low Earth orbit. The partially reusable P6
is a full-scale, low-fidelity prototype of the two-stage, pressure-fed
NLV and is serving as a pathfinder for evaluating new vehicle
technologies and efficient field site operations.
Designed and built
by Garvey Spacecraft Corporation (GSC) and California State
University, Long Beach (CSULB) under the California Launch Vehicle
Education Initiative (CALVEIN), the 26.7 foot-long P6 consists
of a refurbished NLV first stage prototype (the Prospector
5 that flew last December), an interstage, a second stage
simulator and a graphite/epoxy composite payload fairing. The
research team conducted their test operations at the Mojave
Test Area that is owned and operated by the Reaction Research
Society.
Flight videos:
The primary objective
for this initial P6 flight test was validation of the CALVEIN
team's ability to develop and handle a full-scale NLV. Maximum
altitude achieved on the flight was slightly under 3000 feet.
Of significance for advocates of responsive space operations
was the demonstration of vehicle delivery, integration, payload
installation, propellant loading, launch, recovery and shipment
back to the CSULB campus in a single day.
P6 being
erected to launch position (Photo by Dave Allday)
P6 on
the launch rail during pre-launch preparation (Photo by Joe
Mullin)

P6
at engine ignition (Photo by Dave Allday)

P6
during launch (Photo by Joe Mullin)

P6
in flight (Photo by Joe Mullin)
The P6 features several
design enhancements over previous prototypes, including the
CALVEIN team's first implementation of a stage attachment and
separation system, as well as multiple applications of composite
materials for structural bulkheads and fins. The P6 flight also
continued the CALVEIN practice of manifesting student payloads
from across the country. CSULB experiments included a mini-DV
camera sponsored by the student chapter of the AIAA that captured
on-board video of the entire flight sequence, as well as a real-time
telemetry system that adapted commercial off-the-shelf Wi Fi
technology to downlink key propulsion system parameters. In
addition, a measurement logging package provided by Montana
State University recorded acceleration, pressure and temperature
data that is already being used to assess the vehicle's performance.
P6
stages after successful parachute deployment (Photo by Dave
Allday)

P6
first stage just prior to landing (Photo by Joe Mullin)
With the successful
recovery of the P6, the CALVEIN team is now updating their plans
to reuse the hardware in future flight testing. In parallel
to such full-scale vehicle test and evaluation activities, GSC,
CSULB and other partners are also investigating alternative
"green" hydrocarbon propellant combinations, advanced
engine chambers materials and innovative approaches to payload
accommodations. Previous team achievements include the first-ever
powered flight tests of a liquid-propellant aerospike engine
and composite cryogenic propellant tankage for liquid oxygen.