KC-135

Zero Gravity Trainer


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.

   

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.

Dr. LaPinta helps out as I (Ken Jenks) lose my breakfast
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.


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 )
  • 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


Provided By:
Dan Whipple
whipple@grc.nasa.gov
(216) 433-5859

Kathy Schubert
Multi-Discipline Program Manager
Functional Resource Manager
(216) 433-5331

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



The KC-135 parked in front of the NASA LeRC Hanger.


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.



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.


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.


Other KC-135 Related Pages





 

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.