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KC-135
Zero
Gravity Trainer
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At NASA's Johnson
Space Center, there is a microgravity research aircraft, a KC-135
(a predecessor of the Boeing 707 which is typically used for refueling
military aircraft) nicknamed the "Vomit Comet." The KC-135
is a four-engine turbojet. It is used to fly parabolas
to investigate the effects of "zero" gravity.
Investigators who fly experiments on the KC-135 must
have a valid Air Force Class III medical, with NASA Physiological
Training (which consists of an eight-hour training course and a
high-altitude chamber run for hypoxia symptom training).
The day before the flight a Test Readiness Review
is conducted. The investigators bring the hardware they'll be flying
on the "K-bird" to building 993 at Ellington Field (near
NASA JSC), where safety inspectors review the documentation and
each investigator gives a briefing on his experiment. Typically,
all the other investigators huddle around and watch each other's
briefings. During the briefing, the investigator gives an overview
of the experiment and the equipment, tells about the planned sequence
of events, and describes how the equipment will be mounted inside
the vehicle. (Equipment must be mounted to withstand 9 G crash loads.)
The safety inspectors might ask questions about the medical effects
of the procedures, or about how the wires will be run, etc. They
frequently give the investigators last-minute suggestions for improving
safety or convenience of the experiment. At the end of the inspection,
the investigators are given a go/no-go, or are told what modifications
need to be done before flight.
Later that day, the investigators will have access
to the aircraft to mount their hardware, install any wiring, and
tap into the aircraft's 120 VAC power lines.
The next morning, the aircraft is open at around
7 AM. Investigators arrive, make any last-minute adjustments to
their experiments, then go into building 993. About 8 AM, there
is a pre-flight safety video which reminds investigators about safety
equipment and procedures. After the video, the investigators don
flight suits (if you don't have your own, you'll be issued one)
and heavy boots (ditto). Barf bags are handed out. (The best place
for a barf bag is in the pockets on your chest, sticking out a little
bit, with the top open. When the urge to hurl comes, it will come
fast. Most of the investigators take their anti-nausea drugs, usually
Scop-Dex, a mixture of scopalamine and dexadrine.
About 9:30, the investigators start making their
way out to the aircraft. Ground support equipment (GSE) provides
electrical power and (blessedly) air conditioning to the aircraft
before flight. After a bit of milling around, the investigators
take their seats at the rear of the aircraft, while Linda Billica
and Bob Williams direct traffic and generally help out. Dr. LaPinta
takes his seat. The NASA videographers check their camera mountings
(if any), and strap in. Bob is the head of the team, Linda is his
able assistant. Dr. LaPinta provides medical assistance before,
during and after the flight. There's almost always a NASA photographer
on board, sometimes two, for taking still photos and video during
the flight. There's a pilot and a co-pilot up front, but we investigators
never see them.
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The accomodations are spartan. We investigator s sit in military-style
seats at the back of the plane. There is one potty (but you don't
want to use it during zero-G). There's little air conditioning at
the back of the plane, and the lighting is dim. The investigators
sit around and joke during taxi and take-off. No in-flight meals,
and Bob makes a crummy stewardess. Dr. LaPinta has a supply of hard
candy, which helps take your mind off your stomach. Take-off usually
happens around 10 AM. |
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Dr. LaPinta helps out as I (Ken Jenks)
lose my breakfast
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After departing Ellington Field (EFD)
to the south, the plane flies out over the Gulf of Mexico, climbing
to around 26,000 MSL (altitude above mean sea level), and 350 KIA
(knots indicated airspeed). The yaw and roll autopilots are engaged,
and the pitch axis autopilot is disengaged. The pilot then pulls the
nose up steadily to a maximum of 1.8 G, pitching up to 45-50 degrees.
The airspeed drops off. The pilot pushes the stick forward and comes
back on the thrust, taking the two outboard engines to idle, while
the thrust of the two inboard engines control the fore/aft acceleration
to zero. The pilot watches the reading on the accelerometer, using
miniscule control inputs to keep it at zero. Over the top of the parabola,
the pilot pushes the stick forward to hold the acceleration to zero.
The top of arc comes at 36,000 MSL, with 150-170 KIA. The pilot continues
to pitch over until the aircraft is 45 degree nose down. Thrust is
steadily increased until back to 350 KIA, at which point the pilot
pulls back on stick, bringing acceleration up to 1.8 G. The maneuver
ends back at 26,000 MSL, 350 KIA. Wind from the nose or tail varies
the parabola somewhat. |
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Provided By The Glenn Research Center Aviation Safety Committee
The following information is for use when designing
or calculating information for the safety review of experiments
flying on the KC-135 aircraft.
- Standard day conditions at 0 ft. altitude (NACA Report 1235
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- Pressure 2116.216 lbf/ft**2 (14.696 psia) (29.921 inches Hg)
- Temperature 59 deg F
- Density 0.076475 lbm/ft**3
Design Requirements
This is a very brief outline. See the Glenn Safety
Manual and other applicable documents for the full requirements.
Structural and mechanical design of experiment hardware
should provide a minimum factor of safety of 1.0 against yield failure
of the material and/or 1.5 against the ultimate failure of the material,
whichever is limiting. Components prone to brittle failure (such
as optical windows) shall be designed with a minimum factor of safety
of 10.0 against the ultimate strength of the material. The worst
case operating temperature expected to be seen by the material must
be taken into account.
Each pressure vessel and pressurized system shall
be designed to 4 times the Maximum Allowable Working Pressure (MAWP)
and certified by testing to 1.5 MAWP. Pressure relief devices based
on the MAWP and having a flow capability suitable for preventing
overpressurization must be used. Systems inherently low in energy
or commercial systems having a record of operation without serious
incident need only to be shown to work without failure when exposed
to the worst case operational conditions.
Electrical systems shall be designed and documented
with components and wiring suitable for the expected voltages and
currents. Each circuit shall have one or more overcurrent protective
devices to prevent exceeding the design limits. Circuit steady-state
loads shall not exceed 80% of the overcurrent protective device
limit.
The Qualified Operators List (QOL) required for the
safety permit will consist of the flight crew manifest. If any non-flying
persons will operate the equipment for ground checkout they should
be added to the QOL.
- JSC KC-135 (Tail 931)
- Aero Loads
- All experiments are internal
- Structural Loads
- Mounted in cabin
- Forward 9g
- Aft 3g
- Lateral 2g
- Up 2g
- Down 6g
Free float or stowed for takeoff/landing experiments need only meet
worst case microgravity loads (3g any axis) but must meet cabin
mount loads when stowed. (Design to cabin loads or stow in approved
container)
Cabin Volume
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Provided By:
Dan Whipple
whipple@grc.nasa.gov
(216) 433-5859
Kathy Schubert
Multi-Discipline Program Manager
Functional Resource Manager
(216) 433-5331
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Use 4346 ft**3 for calculations
Exchange rate is 3 minutes for entire volume
Cabin Pressure
Nominal cabin altitude is 8000 ft (10.9 psia) during parabolic
maneuvers
Worst case if depressurized use 3.5 psia
Cabin Temperature
Normal operating temperature 50-80 deg F
Ground temperatures may exceed these limits
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The KC-135 parked in front of the NASA
LeRC Hanger.
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During a flight, which lasts about two hours, total, we usually
fly 40 parabolas. In this aircraft,
tail number NASA 930, we've done as many as 101, depending on fuel
and gross weight limitations. More parabolas mean more flexing of
the airframe and more stress. We could fly 200 maneuvers, but we'd
use the airplane up.
After the flight, we fly back to EFD, usually arriving
around 12. We change out of our flight suits, and we talk about
how our experiments went. (We don't usually talk about who got sick
and who didn't.) The more adventurous (or more masochistic) go to
Pe-Te's Cajun Barbeque for lunch. The investigators remove their
equipment from the aircraft -- it must be out by about 3 PM.
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The KC-135 operates out of NASA
Glenn several weeks each year in support of Lewis' ground-based
microgravity research. Some flights include astronauts participating
in crew training so that they can have low-g experience with experiment
hardware prior to shuttle missions.
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Interesting fact about the KC-135
- The KC-135 Vomit Comet was used to film the weightless
scenes for the movie Apollo 13. Ron Howard, his crew, and
the cast spent more than half a year renting space and time on
the plane to produce the movie.
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Other KC-135 Related Pages
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Flights
from Glenn Research Center
29 October 2001
18 March 2002
15 April 2002
13 May 2002
8 July 2002
19 August 2002
9 September 2002
Flights from Johnson Space Center
1 October 2001
15 October 2001
22 October 2001
5 November 2001
7 January 2002
28 January 2002
4 February 2002
11 February 2002
1 April 2002
22 April 2002
29 April 2002
24 June 2002
15 July 2002
5 August 2002
26 August 2002
23 September 2002
In addition to the above listed weeks, the aircraft
is scheduled to support other programs with reduced gravity flights from
the Johnson Space Center on the following weeks:
14 January 2002
25 February 2002
4 March 2002
11 March 2002
25 March 2002
8 April 2002
6 May 2002
22 July 2002
29 July 2002
12 August 2002
16 September 2002
These weeks may be available to code UG investigations
when the primary organization is unable to fill the aircraft for a particular
flight week. If you wish to schedule an investigation for flight at GRC
or JSC, please contact either
Eric Neumann
eric.neumann@grc.nasa.gov,
(216)433-2608,
or
Jim Withrow
james.withrow@grc.nasa.gov,
(216) 433-8315.
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