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C = Captive Carry
L = Launch
G = Glide
P = Powered
The first letter represents the intended mission for
the flight and the second letter, if present, represents
the actual mission flown. For example, first glide will
for the space ship will be 03G. If the flight aborts
or doesn't release for whatever reason, the nomenclature
becomes 03GC.
| Flight |
66L / 17P
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| Date: |
04 Oct 04
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Flight
Time: |
1.6 hour / 24 min |
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| White
Knight Pilot: |
Melvill |
White Knight Copilot: |
Stinemetze |
SpaceShipOne
Pilot:
|
Binnie |
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High
Chase Alpha Jet Crew:
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Van der Schueren /
Johnson
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| High
Chase-Starship Crew: |
Karkow
/ Scherer |
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| Low
Chase-Extra Crew: |
Coleman / Bird |
| Objectives: |
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Second
X-prize flight: again ballasted for 3 place &
100 kilometer goal (328,000 ft)
(We also really wanted to break the X-15 354kft
record)
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| Results: |
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| A very large crowd
of dignitaries and X-prize guests…along
with a whole lot of local folks cheered the
White Knight turbojet with SS1 tagging along
to a 6:49 a.m. PST takeoff. The launch altitude
this flight was 47,100 feet. At 7:49 a.m. PST,
flight engineer Matt Stinemetze released the
spaceship and test pilot Brian Binnie immediately
fired the hybrid rocket motor. This ignition
was so quick that Mike & Matt actually heard
the rocket burn from inside the WK. The rocket
burn lasted for 83 seconds boosting the vehicle
to more than 3.09 Mach or 2186 miles an hour.
At motor burn out, SpaceShipOne was at 213,000
feet and from there coasted the rest of the
way into space reaching an apogee of 367,500
(radar) feet (112 Km). Brian feathered the spaceship
as dynamic pressure approached zero during ascent.
Like Mike on 16P, Brian used a digital camera
to shoot pictures (one of Brian’s photos
later appeared on the cover of Aviation Week).
He also conducted a series of zero-g experimental
flight tests of a small paper SpaceShipOne model.
Binnie experienced weightlessness for approximately
3 ½ minutes as the vehicle slowly decelerated
to apogee, and then began its fall towards the
atmosphere. Maximum Mach during entry was 3.25.
During the descent, the pilot experienced a
peak deceleration of 5.4 G's at about 105kft
altitude. Brian reconfigured the vehicle back
to a glider by commanding feather retraction
at 51,000 feet and over the next 18 minutes
enjoyed a leisurely descent to a graceful landing
at Mojave, thus closing the book on our Tier
One program. This historic flight not only broke
the X-15 record by 13,000 ft, and won the X-prize,
but was a picture perfect ending to the program.
No anomalies were noted on the flight and SpaceShipOne
returned with no maintenance squawks. This last
Tier One flight was a testament to what training
and good old-fashioned hard work can do.
The 13 month, 17-flight SpaceShipOne flight
test program included just six rocket powered
flights, three of which flew to space (above
100 Km). In comparison, the X-15 program (which
included 3 test aircraft) took 3 years 4 months,
and 110 flights to reach 50 miles altitude (80.5
Km), and 4 years 4 months to reach Space (100
Km altitude).
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| Flight |
65L / 16P
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| Date: |
29 Sept 04
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Flight
Time: |
1.6 hour / 24 min |
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| White
Knight Pilot: |
Binnie |
White Knight Copilot: |
Stinemetze |
SpaceShipOne
Pilot:
|
Melvill |
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High
Chase Alpha Jet Crew:
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Van der Schueren /
Johnson
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| High
Chase-Starship Crew: |
Karkow
/ Scherer |
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| Low
Chase-Extra Crew: |
Coleman / Bird |
| Objectives: |
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| First
X-prize flight: ballasted to simulate 3 place,
& to exceed 100 kilometers (328,000 ft) |
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| Results: |
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| Greeted early
in the morning by thousands of eager X-prize
onlookers, the White Knight turbojet launch
aircraft took off at 7:12 a.m. PST, carrying
SpaceShipOne under its fuselage to an altitude
of 46,500 feet. At 8:10 a.m. PST, flight engineer
Matt Stinemetze released the spaceship and test
pilot Mike Melvill quickly fired the hybrid
rocket motor. The rocket burn lasted for 77
seconds, boosting the vehicle to more than 2.92
Mach or 2110 miles an hour. At motor burn out,
SpaceShipOne was at 180,000 feet and from there
it coasted the rest of the way into space reaching
an apogee of 337,700 (radar data) feet (103
Km). At 60 seconds into the burn, very large
roll-rates were experienced (see description
below). The vehicle entered into a right rolling
ascent at an initial average roll rate of 190
°/sec. Since the ship was in thin air and
quickly leaving the atmosphere, it was not possible
to stop the rolls using only aerodynamic flight
controls. Melvill did input aerodynamic corrective
controls and was able to lower the roll rate
to 140°/sec before leaving the atmosphere.
Later, after feathering the wing/tail, he used
the reaction control system (RCS) to damp the
roll rate. Mike was able to completely remove
the rates before reaching apogee. He then used
a hand-held digital camera to shoot some pictures
out the windows. Melvill experienced weightlessness
for approximately 3 ½ minutes. The supersonic
feathered atmospheric entry was smooth, with
only small oscillations. During the descent
the spaceship accelerated to Mach 3.0. At max
q, approximately 105kft altitude, Mike experienced
a peak deceleration of 5.1 G's. Mike reconfigured
the vehicle back to a glider by commanding feather
retraction at 61,000 feet and over the next
18 minutes enjoyed a leisurely descent to a
graceful landing at Mojave, the Nation's first
inland Space Port. Mike now holds the world
record for the most aileron rolls during a vertical
climb! :) SpaceShipOne returned with no maintenance
squawks.
SpaceShipOne Flight
16P Anomaly:
Highly publicized in the media, the rolls near
the end of the motor burn certainly got our
attention. Detailed analysis determined that
the rolls resulted from a mild thrust asymmetry,
which was unable to be offset by pilot inputs
at a flight condition of low directional stability.
This flight condition had not been tested on
previous flights. The low directional stability
occurs only at high mach #’s and at very
low (zero or negative) angles of attack. On
earlier flights the aircraft still had some
lift at high mach numbers and did not approach
the low angle of attack regime. On 16P, because
Mike did such a great job of turning the corner
early in the burn, the later segments of the
burn had to be at near zero lift to point the
trajectory in the desired direction. At this
condition around mach 2.7 the airplane was excited
in yaw and then the high dihedral effect resulted
in a rolling departure from controlled flight.
The fix to this problem that allowed a smooth
boost 5 days later on 17P, was to fly a slightly
less aggressive initial pull-up. This allowed
Brian to avoid the low angle of attack regime
when at high Mach. The characteristics of excessive
dihedral effect and high-Mach low directional
stability will be corrected on future spaceship
designs. |
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| Flight |
60L / 15P
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| Date: |
21 June 04
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Flight
Time: |
1.6 hour / 24 min 05sec |
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| White
Knight Pilot: |
Binnie |
White Knight Copilot: |
Stinemetze |
SpaceShipOne
Pilot:
|
Melvill |
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High
Chase Alpha Jet Crew:
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Van der Schueren /
Johnson
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| High
Chase-Starship Crew: |
Karkow
/ Scherer |
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| Low
Chase-Extra Crew: |
Coleman / Bird |
| Objectives: |
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| First
commercial astronaut flight by exceeding 100 kilometers
(328,000 ft) |
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| Results: |
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| Cheered down the
runway by onlookers, the White Knight turbojet
launch aircraft took off at 647 a.m. PST, carrying
SpaceShipOne under its fuselage to an altitude
of 47,000 feet. At 750 a.m. PST, flight engineer
Matt Stinemetz released the spaceship and test
pilot Mike Melville immediately fired the hybrid
rocket motor. The rocket burn lasted for 76
seconds rocketing the vehicle to more than 2.9
Mach or 2150 miles an hour. At motor burn out,
SpaceShipOne was at 180,000 feet and from there
coasted the rest of the way into space reaching
an apogee of 328,491 feet. Melvill experienced
weightlessness for approximately 3 ½
minutes as the vehicle slowly decelerated to
apogee and then yielding to the pull of gravity
commenced its historic return to earth in the
craft's unique entry or feathered configuration.
During the descent the pilot experienced forces
greater than 5.0 G's as the vehicle accelerated
again to 2.9 Mach. Melvill reconfigured the
vehicle back to a glider at 57,000 feet and
over the next 20 minutes enjoyed a leisurely
descent to a graceful landing at Mojave, the
Nation's first inland Space Port.
SpaceShipOne Flight
15P Anomaly:
As mentioned in the post-flight press conference,
during SpaceShipOne's historic flight to 100
kilometers on 21 June 2004 there was a flight
control malfunction. Late in the boost phase,
the vehicle s primary pitch trim control was
lost. Scaled views any flight control system
anomaly as a serious matter, but to guard against
these problems, the vehicle has redundancy on
all flight-critical systems, including pitch
trim. So when the failure occurred, test pilot
Mike Melvill switched to the backup system and
continued the planned mission. However, the
resulting trajectory excursion had two effects.
One, the vehicle didn't climb as high as planned
and two, the space ship re-entered south of
the intended recovery point. This latter effect,
while undesirable, was well within the vehicle's
glide capability and SpaceShipOne had no difficulty
flying back to Mojave Space Port for a normal
landing. |
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| Flight |
56L / 14P
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| Date: |
13 May 04
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Flight
Time: |
1.5 hour / 20 min 44sec |
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| White
Knight Pilot: |
Binnie |
White Knight Copilot: |
Stinemetze |
SpaceShipOne
Pilot:
|
Melvill |
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High
Chase Alpha Jet Crew:
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Van der Schueren /
Johnson
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| Low
Chase-Duchess Pilot: |
Siebold
/ Moore |
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| Objectives: |
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| The third
powered flight of SpaceShipOne. 55 seconds motor
burn time. Handling qualities during boost and
performance verification. Reaction control system
use for reorientation to entry attitude. Supersonic
feather stability and control. |
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| Results: |
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Launch
conditions were 46,000 feet and 120 knots. Motor
light off occurred 10 seconds after release and
the vehicle boosted smoothly to 150,000 feet and
Mach 2.5. Subsequent coast to apogee of 211,400
feet. During a portion of the boost, the flight
director display was inoperative, however the
pilot continued the planned trajectory referencing
the external horizon. Reaction control authority
was as predicted and the vehicle recovered in
feather experiencing 1.9M and 3.5G’s. Feather
oscillations were actively damped by the pilot
and the wing was de-feathered starting at 55,000
feet. The onboard avionics was re-booted and a
smooth and uneventful landing made to Mojave.
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| Flight |
53L / 13P
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| Date: |
8 Apr 04
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Flight
Time: |
1.3 hour / 16 min 27
sec |
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| White
Knight Pilot: |
Binnie |
White Knight Copilot: |
Stinemetze |
SpaceShipOne
Pilot:
|
Siebold |
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| High
Chase-Starship Crew: |
Karkow / Schere |
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High
Chase Alpha Jet Crew:
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Van der Schueren /
Johnson
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| Low
Chase-Extra Pilot: |
Melvill
/ Coleman |
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| Objectives: |
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The second
powered flight of SpaceShipOne. 40 seconds motor
burn time. Handling qualities during boost, through
transonic and supersonic. Reaction control system
functionality in-flight and feather configuration
stability during transonic re-entry. Evaluation
of radar tracking capability.
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| Results: |
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Launch
conditions were 45,600 feet and 125knots. A planned
immediate motor ignition was delayed about 2 minutes
to evaluate a shock induced stall buffet resulting
in an ignition altitude of only 38,300 feet. The
40 second rocket boost was smooth with good control.
Pilot commented that the motor was surprisingly
quiet; however the boost was heard by ground observers.
Burnout occurred at 1.6M and apogee was over 105,000
feet. There was no noted flight control flutter
or buzz during the climb. Feather recovery was
nominal. Maximum feathered speed on entry was
0.9 Mach. The wing was de-feathered and locked
by 40,000 feet. Handling quality assessments during
descent were satisfactory and a smooth landing
made to runway 30 at Mojave. All video and tracking
systems performed well with spectacular footage
obtained onboard, from chase and from ground stations.
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| Flight |
49L / 12G |
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| Date: |
11 MAR 04 |
Flight
Time: |
1.3 hours / 18 mins
30 secs |
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| White
Knight Pilot: |
Binnie |
White Knight Copilot: |
Stinemetze |
| White
Knight Flt Engineer: |
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| SpaceShipOne
Pilot: |
Siebold |
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| High
Chase-Starship Pilot: |
Karkow |
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| Low
Chase-Extra Pilot: |
Melvill
/ Coleman |
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| Objectives: |
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| The twelfth
flight of SpaceShipOne. Objectives included: pilot
proficiency, reaction control system functionality
check and stability and control and performance
of the vehicle with the airframe thermal protection
system installed. This was an unpowered glide
test. |
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| Results: |
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Launch conditions were 48,500 feet and 125 knots.
All systems performed as expected and the vehicle
landed successfully while demonstrating the maximum
cross wind landing capability.
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| Flight |
43L / 11P |
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| Date: |
17 Dec 03 |
Flight
Time: |
1.2 hours / 18 mins
10 secs |
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| White
Knight Pilot: |
Siebold |
White Knight Copilot: |
Bird |
| White
Knight Flt Engineer: |
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| SpaceShipOne
Pilot: |
Binnie |
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| High
Chase-Starship Pilot: |
Karkow |
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| Low
Chase-Extra Pilot: |
Melvill
/ Coleman |
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| Objectives: |
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| The eighth
flight of SpaceShipOne and first powered flight.
15 second burn of the rocket motor and supersonic
flight. Motor light off at altitude and inflight
engine performance. Vehicle handling qualities
through transonics and feather performance from
altitude. |
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| Results: |
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| Launch
conditions were 47,900 feet and 112 knots. Motor
light off was achieved at 44,400 feet and 0.55M.
Burnout occurred at 1.2M and apogee was 67,800
feet. There was no noted flight control flutter
or buzz during the climb. Feather recovery exhibited
a +/-30 roll initially and then settled down into
the familiar falling bathtub mode. The wing was
de-feathered and locked by 35,000 feet. A nominal
landing pattern was flown but touchdown caused
the left main gear to collapse and the vehicle
rolled to a stop off the runway in the soft sand.
Although the damage was not major, repairs are
expected to take approximately three weeks to
complete.
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| Flight |
42L / 10G |
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| Date: |
4 Dec 03 |
Flight
Time: |
1.3 hours / 13 mins
14 secs |
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| White
Knight Pilot: |
Siebold |
White Knight Copilot: |
Stinemetz |
| White
Knight Flt Engineer: |
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| SpaceShipOne
Pilot: |
Binnie |
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| High
Chase-Starship Pilot: |
Karkow |
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| Low
Chase-Extra Pilot: |
Melvill
/ Coleman |
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| Objectives: |
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| The seventh
glide flight of SpaceShipOne and new pilot check
out. Full functional check of the propulsion system
by cold flowing nitrous oxide. Completed airspeed
and positive and negative G-envelope expansion.
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| Results: |
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| Launch
conditions were 48,400 feet and 115 knots. All
propulsion components, displays and functionality
performed as designed. The feather was extended
after a 4G pull-up to the vertical at 24,500 feet
and rudder used to induce sideslip and yaw rates
while "going-over-the-top". The vehicle
recovered to a stable attitude and descent after
only a single oscillation. The landing pattern
was flown following established procedures resulting
in a satisfactory touchdown. |
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| Flight |
41L/09G |
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| Date: |
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19-Nov-03 |
Flight
Time: |
2.1 hours / 12 mins
25 secs |
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| White
Knight Pilot: |
Binnie |
White Knight Copilot: |
Bird |
| White
Knight Flt Engineer: |
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| SpaceShipOne
Pilot: |
Melvill |
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| High
Chase-Starship Pilot: |
Siebold |
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| Low
Chase-Duchess Pilot: |
Coleman
/ Stinemetze |
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| Objectives: |
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| The sixth
glide flight of SpaceShipOne. Test pilot Mike
Melvill's first flight with the enlarged tails.
Emergency aft CG handling qualities eval and simulated
landing exercise with the new tail configuration.
Airspeed and G envelop expansion and dynamic feather
evaluation. |
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| Results: |
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| Launch
conditions were 48,300 feet and 115 knots. Satisfactory
vehicle handling characteristics at the emergency
CG limit. Melvill reported improved stability,
improved control powers and improved stick forces
throughout the flight profile. The feather was
extended after a 3G pull-up to the vertical at
30,000 feet. The vehicle recovered to a stable
attitude and descent after a few mild oscillations.
The landing pattern was flown at a higher airspeed
than previous flights which allowed for a more
controlled flare and landing at the nominal touchdown
point. |
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| Flight |
40L/08G |
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| Date: |
14-Nov-03 |
Flight
Time: |
1.4 hours / 19 mins
55 secs |
| White
Knight Pilot: |
Binnie |
White Knight Copilot: |
Stinemetze |
| White
Knight Flt Engineer: |
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| SpaceShipOne
Pilot: |
Siebold |
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| High
Chase-Starship Pilot: |
Karkow |
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| Low
Chase-Duchess Pilot: |
Melvill/
Coleman |
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| Objectives: |
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| The fifth
glide flight of SpaceShipOne. New pilot checkout
flight. Stability and control testing with the
new extended horizontal tails. Tests included
stall performance at aft limit CG and evaluation
of the increased pitch and roll control authority.
Other objectives included additional testing of
the motor controller (MCS) and handling qualities
in feathered flight. |
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| Results: |
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| Launch
conditions were 47,300 feet and 115 knots. Satisfactory
stability and control at aft limit CG. A notable
improvement in control power, particularly in
roll. Handling qualities into and out of feather
remained excellent with good nose pointing ability.
Adjusted landing pattern altitudes resulted in
a touchdown at the targeted runway aim-point.
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| Flight |
38L/07G |
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| Date: |
17-Oct-03 |
Flight
Time: |
1.1 hours/ 17 mins
49 secs |
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| White
Knight Pilot: |
Siebold |
White Knight Copilot: |
Bird |
| White
Knight Flt Engineer: |
Moore |
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| SpaceShipOne
Pilot: |
Melvill |
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| High
Chase-Starship Pilot: |
Binnie |
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| Low
Chase-Extra Pilot: |
Coleman |
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| Objectives: |
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| Fourth
glide flight of SpaceShipOne. Primary purpose
was to examine the effects of horizontal tail
modifications at both forward and mid-range CG
locations (obtained by dumping water from an aft
ballast tank between test points). The tail modifications
included a fixed strake bonded to the tail boom
in front of the stabilator and a span-wise flow
fence mounted on the leading edge of each stab
at mid-span. (See the write up under the SPACESHIPONE
GROUND TEST section that describes our Ford-250
wind tunnel which was used to help derive the
current flight configuration). Other test objectives
included a functional check of the rocket motor
controller, ARM, FIRE and safing switches as well
as the oxidizer dump valve. Additional planned
maneuvers included full rudder pedal sideslips
and more aggressive nose pointing while in the
feathered configuration. |
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| Results: |
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| Launch
conditions were 46,200 feet and 115 knots and
produced a clean separation. The tail performance
was examined by flying "longitudinal stability"
points between stall and 130 knots and showed
considerable improvement of the airfoil's lift
coefficient as well as its post stall characteristics.
No vehicle pitch up tendency was noted as the
main wing now stalls first. Real time video of
the tufted tails fed back down to mission control
helped considerably in assessing the performance
of these aerodynamic improvements. More aggressive
maneuvering in the feather made it evident that
the pilot could readily point the vehicle's nose
where desired and all rocket motor functionality
tests were satisfactory.
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| Flight |
37L / 06G |
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| Date: |
23-Sep-03 |
Flight
Time: |
1.5 hours / 12 mins
15 secs |
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| White
Knight Pilot: |
Siebold |
White Knight Copilot: |
Stinemetz |
| White
Knight Flt Engineer: |
Johnson |
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| SpaceShipOne
Pilot: |
Melvill |
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| High
Chase-Starship Pilot: |
Karkow |
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| Low
Chase-Duchess Pilot: |
Binnie |
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| Objectives: |
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Third
glide flight of SpaceShipOne. Aft CG flying qualities
and performance evaluation of the space ship in
both the glide and re-entry or "feather"
mode. Glide envelope expansion to 95% airspeed,
100% alpha and beta and 70% loadfactor. More aggressive
post stall maneuvering and spin control as a glider
and while feathered. Nitrous temperature control
during climb to altitude and performance of upgraded
landing gear extension mechanism and space-worthy
gear doors. |
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| Results: |
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| Launch
conditions were 46,800 feet and 115 knots and
produced a clean separation. First stall entry
maneuver resulted in an un-commanded nose rise
before reaching the wing stall angle of attack.
Lateral/directional controls were used in conjunction
with forward stick to effect recovery. This aft-cg
stall characteristic was worse than predicted
and will likely require aero modifications to
fix. The feather entry was not explored and the
rest of the glide flight used to assess the handling
qualities of the vehicle leading to an uneventful
landing. The White Knight's heating system was
able to keep the Spaceship's nitrous oxidizer
conditioned during climb, such that the maximum
N2O pressure variation was less than 6 psi.
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| Flight |
32L / 05G |
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| Date: |
27-Aug-03 |
Flight
Time: |
1.1 hours /10 mins
30 secs |
| White
Knight |
Pilot: |
Binnie |
Copilot: |
Bird |
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| SpaceShipOne |
Pilot: |
Melvill |
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| High
Chase-Starship |
Pilot: |
Siebold |
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| Low
Chase-Duchess |
Pilot: |
Karkow |
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| Objectives: |
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| Same objectives
as the aborted flight 31LC/04GC earlier today.
Second glide flight of SpaceShipOne. Flying qualities
and performance in the space ship re-entry or
"feather" mode. Pilot workload and situational
awareness while transitioning and handling qualities
assessment when reconfigured. As a glider, stall
investigation both at high and low altitude and
envelope expansion out to 200 kts and 4 G's. More
aggressive, lateral directional characteristics
including adverse yaw, roll rate effectiveness
and control, including 360 degree aileron roll,
and full rudder side slips. |
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| Results: |
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| Clean separation
from launch at 48,200 feet and 105 knots, 8 miles
north east of Mojave. First maneuver was a full
stall, resulting in 70 KEAS at about 19 alpha.
Good lateral control at minimum speed with ailerons
and even better with rudder allowing timely control
of roll-off tendencies. Second maneuver was unlocking
the wing and commanding the full feathered mode
(65 deg wing/tail jackknife). Transition to the
feather mode occurred at 43,000 feet and 90 knots.
As the tail booms and aft wing transitioned upward,
the vehicle body smoothly pitched up and then
returned to an approximately level pitch attitude
during about 70 seconds of fully-feathered descent.
The pilot noted the expected airframe buffeting
and found the ship was very stable at an angle
of attack of about 70 degrees. He was able to
turn the vehicle both left and right with either
rudder or aileron controls. As expected, full
pitch control inputs had little effect on the
flight path. Average sink rate was greater than
10,000 feet per minute. Reconfiguration back to
the normal glider mode occurred at 30,000 feet
with a positive wing lock indicated by on-board
instrumentation and cameras. Third and forth maneuvers
were the airspeed and G envelope expansion which
were flown without incident. Fifth maneuver was
roll-performance, which resulted in a low amount
of adverse yaw but lower roll rates | |