Skip navigation links
NASA Glenn Research Center

+ NASA Home
+ Glenn Home
Go
ABOUT NASA NEWS AND EVENTS MULTIMEDIA MISSIONS POPULAR TOPICS MyNASA

Multidisciplinary
Design, Analysis, and
Optimization Branch
Home
About Us
Top Stories
Reference Material
Education
Search Glenn Research Center
Go
EDUCATIONAL ACTIVITIES: THE NASA AEROQUIZ

 
Week of 6/7/99:
 
Q: During Apollo 14's outbound flight to the moon, astronauts Shepard, Mitchell, and Roosa had trouble docking their command module to the lunar module -- a maneuver necessary to extract it from the Saturn third stage. They did finally dock with it, and they avoided having to fly a simplified lunar reconnaissance mission without a landing. But there were concerns that the docking problem could occur a second time: when Shepard and Mitchell were coming back from the moon's surface. What contingency plans did NASA have in the event of a failed dock?
 
A: In the event of a docking failure, Shepard and Mitchell would have had to suit up, go outside, tether the spacecraft together, and transfer themselves and all of the moon rocks to the command module. This emergency procedure was practiced in water tank simulations.
 
No one got the correct answer!
- The Aeroquiz Editor

 

 
Week of 6/14/99:
 
Q: In order to comply with Federal Aviation Regulations, a commercial airplane must satisfy landing gear strength requirements. Drop tests are performed in controlled laboratory settings, where the gear to be tested is placed in a mechanical jig. The jig slams the gear down onto a surface with a force and speed comparable to an actual aircraft landing. How is the forward speed of the aircraft simulated in these tests?
 
A: In a drop-style aircraft landing gear test, the wheel/tire assembly is rotated at a high speed by an electric motor in the reverse direction with respect to normal tire rotation due to ground contact. The rotation speed is equal to the expected rpm of the tire after contact with the runway at the desired landing speeds to be simulated in the test. In such a test, the wheel/tire assembly is connected to the motor by a chain/sprocket arrangement.
 
Congratulations to Stephen W. Jackson.
 

 
Week of 6/21/99:
 
Q: The first really serious effects of aerodynamic compressibility on airplanes were encountered in high-speed dives of fighter airplanes in World War Two. When pilots put their airplanes in steep, terminal velocity dives starting from about 30,000 feet, they were often unable to recover. In these dives, supersonic flow and shock waves formed on the upper surface of the relatively thick wings, causing flow separation. The separated flow, in turn, reduced the elevator effectiveness. The control force necessary to recover from the dive was sometimes beyond the strength of the pilot. At times, however, one of the things that sometimes allowed pilots to pull out of these dives was the higher air temperature encountered at lower altitudes. Why?
 
A: At lower altitudes and higher air temperatures, the speed of sound is faster than it would be in the thin air at higher altitudes, which is well known to be colder. The speed of an aircraft as a percentage of the speed of sound is lower at lower altitudes and/or sea level, which means a reduction or elimination of shock waves, supersonic airflow, and control-reducing airflow separations.
 
Congratulations to Stephen W. Jackson.
 

 
Week of 6/28/99:
 
Q: When we think of Harley-Davidson, we usually think of style, function, sound, feel, chrome, a legendary heritage, and the open road. Would you think of flying at 330,000 feet at speeds approaching Mach five? Why?
 
A: Raytheon Aircraft currently manufactures the AQM-37C: a small, supersonic, expendable target missile. It is propelled by the LR64 liquid-fueled rocket motor, made by Harley-Davidson, and is capable of producing 860 pounds of thrust. The AQM-37 provides air-to-air weapons training for pilots or for surface-to-air missile crews. The AQM-37C has recently been upgraded for use as a ballistic missile target. During exercises in 1996, the missile flew at altitudes of 235,000 feet with a range of 105 miles. Terminal velocities were Mach 4. Air launches at Mach 1.5 at an altitude of 50,000 feet extend the envelope to altitudes of 330,000 feet with a range of 265 miles with terminal velocities near Mach 5.
 
Congratulations to Daniel Shedd.
 
If anyone has the H-D catalog number for the LR64, let me know. I'd have the fastest FXSTC on the block!
- The Aeroquiz Editor.

 


USA.Gov - Government Made Easy
 ExpectMore.gov

+ Freedom of Information Act
+ Budgets, Strategic Plans and Accountability Reports
+ The President's Management Agenda
+ NASA Privacy Statement, Disclaimer,
and Accessibility Certification

+ Inspector General Hotline
+ Equal Employment Opportunity Data Posted
Pursuant to the No Fear Act

+ Information-Dissemination Priorities and Inventories
NASA - National Aeronautics and Space Administration
Page Curator: Jeff Berton
NASA Official: Robert Plencner
Last Updated: August 4, 2008