|
ablation
|
Thermal process where the surface
melts or vaporizes at high temperature, thereby absorbing
heat created aerodynamically.
|
|
ablator
|
Surface material that will melt or
vaporize to absorb heat.
|
|
active cooling
|
Process whereby a heat-conductive
fluid circulates between a hot and cool region, drawing off
heat.
|
|
ADP
|
Advanced Development Projects--a
Lockheed group located in California.
|
|
AF or USAF
|
United States Air Force.
|
|
AFB
|
Air Force Base.
|
|
AFFTC
|
Air Force Flight Test Center.
|
|
AFSC
|
Air Force Systems Command, an Air
Force major command during the period of this
narrative.
|
|
analog
|
In the context of this book, a
computer in a
|
|
computer
|
simulator that solves equations of
motion using analogous electrical circuits; that is, it
expresses data in terms of measurable quantities, such as
voltages, rather than by numbers as a digital computer
does.
|
|
AOA
|
Angle of Attack: direction of
relative wind with respect to an aircraft's longitudinal
axis.
|
|
Apollo
|
NASA program to land a human on the
moon and return to earth.
|
|
ARC
|
NASA Ames Research Center.
|
|
ASD
|
Aeronautical Systems Division (Air
Force).
|
|
aspect ratio
|
The ratio of squared airfoil length
(span) to total airfoil area or of airfoil length to its
mean chord (distance from leading to trailing edge). Thus,
an airfoil of high aspect ratio is relatively long with a
relatively short chord, whereas one of low aspect ratio is
comparatively short and stubby.
|
|
attitude
|
The position or orientation of an
aircraft or spacecraft with relation to its axes and some
reference line or plane.
|
|
ballistic
|
Adjective describing the path of a
body launched into a path where it is subject only to the
forces of gravity and drag.
|
|
Ballistic
|
Weight divided by the drag
coefficient times the Coefficient frontal area.
|
|
bank angle
|
Angle between the plane of an
aircraft's wings and the horizon
|
|
boat-tail
|
Shape of the rear of a vehicle whose
cross section decreases from the center to the aft
end.
|
|
C-130
|
Four-engine, turboprop-powered
transport airplane.
|
|
capsule
|
A self-contained, symmetrical
container capable of safely entering the earth's atmosphere
from orbital or higher speeds.
|
|
CD
|
Drag coefficient. A non-dimensional
parameter for measuring drag.
|
|
c.g.
|
Center of gravity--an imaginary
location within an object that identifies its center of
mass.
|
|
ceramic tiles
|
Small blocks of rigid material
(primarily silica) attached to the outside of a gliding
re-entry vehicle that prevent the heat generated by re-entry
speeds from reaching the vehicle structure.
|
|
chase planes
|
Aircraft used to fly close to
research airplanes for purposes of providing the research
pilot with an additional set of eyes for safety
purposes.
|
|
chord
|
The straight-line distance from the
leading to the trailing edge of an airfoil such as a
wing.
|
|
CL
|
Lift coefficient. A non-dimensional
parameter for measuring lift.
|
|
CLS/W
|
Lift coefficient divided by wing
loading. A non-dimensional parameter that allows the glide
performance of several aircraft to be compared at the same
airspeed.
|
|
control laws
|
The relationship between the pilot's
commands and the actual control surface (aileron, elevon,
etc.) movements produced by a flight control system.
|
|
cross range
|
The distance that can be achieved by
a re-entry vehicle (as it enters the atmosphere) in a
direction perpendicular to that of the initial entry
path.
|
|
damp
|
To slow down.
|
|
decouple mode
|
An entry concept that uses a
different deceleration method for entry than for
landing.
|
|
delta wing
|
A wing that has a triangular shape
when viewed from above.
|
|
digital
|
Adjective describing a mechanism,
such as a computer, that expresses data in discrete,
numerical digits.
|
|
dihedral
|
Effect on lifting bodies of sideslip,
producing roll.
|
|
DoD
|
Department of Defense.
|
|
doublet
|
An aircraft control movement from
neutral to a deflected position that is held, then returned
in the opposite direction back to the original neutral
position.
|
|
drag
|
A force that resists motion and is
produced by friction with the atmosphere.
|
|
Dutch roll
|
A complex oscillating motion of an
aircraft involving rolling, yawing, and
sideslipping--so-named from the resemblance to the
characteristic rhythm of an ice skater.
|
|
Dyna-Soar
|
Short for Dynamic Soaring. Name of a
boost-glide research program that was canceled in 1963
before its first flight. The aircraft designation was
X-20A.
|
|
effective dihedral
|
An aircraft aerodynamic
characteristic that makes the airplane roll (rotate around
the longitudinal axis) when a sideslip or side gust is
encountered.
|
|
eyeballs-in
|
A descriptive term used to identify
the direction of a force due to acceleration.
|
|
F-104
|
Air Force century series fighter
built by Lockheed and used as a chase and research airplane
at the Flight Research Center for many years.
|
|
FDL
|
The Air Force Flight Dynamics
Laboratory located at the Wright-Patterson Air Force Base in
Dayton, Ohio.
|
|
FDL-7
|
Seventh re-entry design created at
the FDL.
|
|
FDL-8
|
Eighth re-entry design created at the
FDL.
|
|
fineness ratio
|
The ratio of body length to body
width of an aerodynamic shape.
|
|
flight cards
|
A type of check list in card form
used by pilots and other crew members to track events in a
planned flight test.
|
|
flight path
|
The path of a moving object, usually
measured in the vertical plane relative to the
horizon.
|
|
fly-by-wire
|
A flight control concept that uses
only electrical signals between the pilot's stick and the
control surfaces.
|
|
FRC
|
The NASA Flight Research Center
located at Edwards, California. From 1954 to 1959, the
designation of this organization was the NACA and then the
NASA High Speed Flight Station. In 1976, it became the NASA
Hugh L. Dryden Flight Research Center.
|
|
frontal area
|
The area of an object as projected
onto a plane perpendicular to the flight direction.
|
|
gain
|
Sensitivity with respect to flight
controls or a stability augmentation system.
|
|
HYPER III
|
A light-weight, unpiloted vehicle
built by the NASA FRC and patterned after the FDL-7
shape.
|
|
hypersonic
|
Characterized by speeds of Mach 5 or
greater.
|
|
jack points
|
Designated points marked on the
underside of an aircraft wing to push upward with a
hydraulic jack for the purpose of calibrating strain gages
inside the wing structure.
|
|
LaRC
|
The NASA Langley Research Center
located in Hampton, Virginia.
|
|
L/D
|
Lift to drag ratio.
|
|
Lift
|
A force on an object produced by
aerodynamic reaction with the atmosphere as the object
moves; it acts perpendicularly to the flight
direction.
|
|
limit cycle
|
A run-away oscillation of an aircraft
control surface that occurs when the sensitivity (gain) of
the automatic stabilization system is too high.
|
|
lower flap control horn
|
A small mechanical arm attached to a
lifting body lower flap control surface to which an actuator
control rod is attached.
|
|
LOX
|
Liquid OXygen.
|
|
Mach number
|
The ratio of an object's speed to
that of sound. Mach 1 is the speed of sound at a given
altitude and temperature; Mach 2 is twice the speed of
sound; and so forth.
|
|
Mercury
|
First U.S. manned space capsule
program.
|
|
MLRV
|
Manned Lifting Re-entry Vehicle. An
early NASA Langley Research Center lifting body
design.
|
|
moment
|
A tendency to cause rotation about a
point or axis, as of a control surface about its
hinge.
|
|
MOU
|
Memorandum of Understanding--usually
a simple document with signatures stating the agreed-upon
responsibilities between two or more organizations.
|
|
MSL
|
Mean Sea Level.
|
|
NACA
|
National Advisory Committee for
Aeronautics.
|
|
NASA
|
National Aeronautics and Space
Administration.
|
|
neutral longitudinal stability
|
A flight condition in which an
aircraft that is disturbed in pitch continues to rotate away
from the initial angle of attack at a constant angular rate
without returning.
|
|
non-receding, charring ablator
|
A type of ablator (see above) that
maintains its external dimensions while melting or
vaporizing.
|
|
nose-wheel
|
The point in an aircraft take-off
maneuver at which rotation the pilot commands the aircraft
to rotate its nose upwards, increasing lift so as to depart
the ground.
|
|
notch filter
|
An electronic filter in an aircraft's
automatic control system to remove or obstruct unwanted
frequencies within a narrow band to prevent them from
causing problems with the system.
|
|
on-the-street
|
The time when an agency advertises
(in a request for proposals) that a new job or contract is
planned.
|
|
overdrive
|
Slang term used to describe the 14
percent increase in thrust that was available on the X-24B
rocket engine as compared with that used on previous lifting
bodies.
|
|
PILOT
|
PIloted LOw speed Test. Early name
for the X-24A program.
|
|
PIO
|
Pilot Induced Oscillation--a
situation in flight in which a pilot causes an aircraft to
deviate from the intended path of flight by making excessive
control inputs.
|
|
pitch
|
Angular displacement of a vehicle
such as an aircraft about the lateral axis (i.e., nose up or
nose down).
|
|
plow horse
|
The author's term for chubby lifting
bodies that are capable of carrying large payloads but have
shorter hypersonic cross ranges than race horses (which
see).
|
|
Pregnant Guppy
|
A C-97 cargo airplane modified to
carry an oversized cargo.
|
|
PRIME
|
Precision Recovery Including
Maneuvering Entry. Early designation for the SV-SD or X-23
program.
|
|
projected area
|
The area of an object as projected
onto a horizontal plane parallel with the flight
direction.
|
|
PSTS
|
Propulsion System Test Stand.
|
|
race horse
|
The author's term for streamlined,
slender lifting bodies with smaller payload capacity than
the plow horses (which see) but with very high hypersonic
cross ranges.
|
|
radiative
|
A type of cooling that radiates heat
away from a cooling hot surface.
|
|
ramjet
|
A type of jet engine without any
mechanical compressor, comprised of a specially shaped, open
tube into which the air necessary for combustion is forced
and then compressed by the forward motion of the
aircraft.
|
|
rate limited
|
Term indicating the maximum angular
rate at which an actuator can drive an aircraft control
surface.
|
|
Real Stuff
|
Term (derived from Tom Wolfe's The
Right Stuff) for people who create and service aircraft or
spacecraft for experimental flights rather than fly
them.
|
|
retrofire
|
Short-term rocket ignition with the
thrust pointed in the direction of flight so as to reduce
the speed of an orbiting object and to initiate
entry.
|
|
Reynolds number
|
A nondimensional parameter
representing the ratio of momentum forces to viscous forces
about a body in fluid flow, as in the atmosphere; named for
English scientist Osborne Reynolds (1842-1912); among other
applications the ratio is vital to the use of wind tunnels
for scale-model testing, as it provides a basis for
extrapolating the test data to full-sized test
vehicles.
|
|
Right Stuff
|
A term first coined by Tom Wolfe in
his book of the same title. It refers to pilots and
astronauts who fly experimental aircraft or
spacecraft.
|
|
Rogallo Wing
|
A wing-like parachute design that
enables the parachuting object to move forward as well as
descend.
|
|
roll
|
Rotational or oscillatory movement of
an aircraft or similar body about its longitudinal
axis.
|
|
Roll Reversal
|
An adverse aircraft design condition
in which an aircraft rolls in the opposite direction from
that commanded by the pilot or control surfaces.
|
|
Rotation Speed
|
The minimum speed at which a pilot
can rotate the aircraft nose upward (lift the nose wheel off
the runway) during a take-off roll.
|
|
RPV
|
Remotely Piloted Vehicle--a vehicle
controlled through radio links by a pilot not physically in
the vehicle.
|
|
RTD
|
Research and Technology
Development--an Air Force Organization.
|
|
SAMSO
|
Space and Missile Systems
Organization--an Air Force organization, part of AFSC during
the period covered by this narrative.
|
|
SAS
|
Stability Augmentation
System--electronic control components designed to augment
the stability of an airplane.
|
|
second generation vehicle
|
A vehicle that has benefited from the
previous generation design, development and testing of a
similar vehicle.
|
|
self-adaptive
|
Adjective describing a flight control
concept that samples, then alters, internal electronic
signals to compensate for changing flight conditions.
|
|
semi-ballistic
|
Adjective describing a state in which
an object is subject to a small lifting force in addition to
the predominant forces of drag and gravity.
|
|
Shuttle
|
The winged vehicle developed by NASA
and its contractors to serve as a Space Transportation
System to carry cargo to and from earth orbit.
|
|
side-arm
|
A two- or three-axis control stick
mounted on the controller side of the cockpit and operated
by a pilot's wrist movements.
|
|
sideslip
|
A sideways movement of an aircraft
away from the initial flight path.
|
|
simulator
|
A partial aircraft cockpit connected
to an electronic computer; it allows a pilot to replicate to
a significant degree the flight of an airplane.
|
|
Skunk Works
|
Popular term for a small, highly
efficient design and fabrication organization capable of
creating innovative prototype aircraft in a short period of
time. The Lockheed Advanced Development Projects group was
the first organization to use the term "Skunk Works"
officially to describe its organization.
|
|
span
|
The distance from tip to tip or root
to tip of an airfoil such as an airplane's wing.
|
|
spiral stability
|
A natural aircraft characteristic
that allows the vehicle either to remain in level flight or
to return thereto when upset in roll or bank angle.
|
|
Sputnik 1
|
The first man-made object to be
placed in earth orbit (by the Soviet Union on 4 October
1957).
|
|
strain gage
|
An instrument used to measure the
strain or distortion in a member or test specimen (such as
an aircraft structural part) that is subjected to a
force.
|
|
strakes
|
Wing-like appendages at the aft end
of an aircraft that provide lift or added stability; also
long, flat surfaces attached to the exterior of an
aircraft's skin and aligned with the local free-stream
conditions.
|
|
SV-5
|
Basic configuration of a re-entry
vehicle that led to the SV-5P (X-24A) and SV-SD
(PRIME).
|
|
SV-5J
|
Jet-powered version of the SV-5
configuration. Two were built but neither was flown.
|
|
swashplate
|
A mechanical plate with a universal
joint giving it freedom to pivot in any direction about one
point. Multiple attachment points for control rods in the
plane of the plate allowed flexibility for different
controls in the M2-F1 lifting body.
|
|
test-bed
|
A conventional aircraft that has been
equipped aircraft with some newly designed internal or
external components for in-flight testing.
|
|
Thor-Delta
|
A two-stage rocket using a Thor 1st
stage and a Delta 2nd stage.
|
|
triply
|
Concept of using three parallel
components to redundant accomplish a single function, with
automatic de-selection of any faulty component.
|
|
tufts
|
Short segments of yarn or string
taped to an aerodynamic surface to allow airflow
characteristics to be observed directly or
photographed.
|
|
volumetric efficiency
|
The ratio of total volume to the
surface area of a three-dimensional shape. A sphere has the
highest volumetric efficiency of any shape.
|
|
wedge angle
|
The angle of the aft control surfaces
relative to the flight direction. Large angles produce
shuttlecock-like stability.
|
|
wetted skin
|
The total exposed surface area of any
shape. In an area aircraft, this is all skin area exposed to
the outside airstream.
|
|
wing loading
|
Vehicle weight divided by the area of
the wing.
|
|
X-24C
|
A follow-on proposal to the X-24B to
test advanced air-breathing propulsion.
|
|
yaw
|
Motion of an aircraft or similar
vehicle about the vertical axis (i.e., nose left or
right).
|
|
Y-plane
|
Lateral (left to right) axis of an
aircraft or flight vehicle.
|