Laser Rangefinder
The NEAR Laser Rangefinder (NLR) is an altimeter that uses a
solid-state pulsed laser to measure the distance between the
spacecraft and the surface of the asteroid 433 Eros. It is one of the
five facility instruments onboard the NEAR spacecraft and will make
highly accurate measurements of the asteroid's shape and detailed
surface structure.
The Laser Rangefinder is a bistatic system, meaning that it consists
of separate transmitter and receiver systems. The transmitter uses a
diode-pumped neodymium-yttrium-aluminum-garnet (Nd-YAG) laser built by
the McDonnell-Douglas Corporation, and the receiver uses a compact
reflecting telescope with baffle/door assembly, enhanced hybrid
silicon avalanche photodiode detector, microprocessor controller with
Mil-Std 1553 bus standard interface, and fast gallium arsenide
time-of-flight electronics built by the Johns Hopkins Applied Physics
Laboratory.
Specifications:
General:
Mass: 5 kg
Power: 20.7 W peak, 16.5 W average
Volume: overall TX/RX assembly 37.5 cm (deep) X 21.6 cm (high) X 22.9 cm (wide) inclusive of overhangs;
10.9 X 15.2 X 3.8 cm laser power supply;
7.6 X 2.5 X 14 cm medium voltage power supply
Data rates: commandable, 51 bps or 6.4 bps
Technical:
Laser wavelength: 1.064 mm
Range accuracy requirement: 6 m
Range requirement: 50 km
Inflight range calibration capability
Pulse repetition rate: commandable among 1/8, 1, 2, and 8 Hz
Pulse energy: 15 mJ
Pulse divergence: 235 mrad
Pulse duration: 12 ns
Range gates: two, commandable
Detector threshold: commandable, eight values
Receiver aperture: 8.9 cm
Range quantization level: 31 cm
Predicted range at asteroid acquisition: 150 km
Laser Altimetry
The NLR directly measures the range between the spacecraft and the
asteroid. The transmitter generates a brief laser pulse, and the
instrument measures the time required for the light to reach the
asteroid and return. When the asteroid is 50 km away, light requires
334 millionths of a second to make the round trip. The time-of-flight
measurements will be used to make accurate determinations of the
asteroid's shape and will help to determine its rotational dynamics.
These shape and kinematics measurements, when combined with analyses
of the very precisely tracked spacecraft orbit around the asteroid,
will yield information on its internal density structure. These data
may address the fundamental question of whether the asteroid is a
homogeneous body or an aggregate of distinctly different bodies.
Laser altimetry complements in several ways the visible and
near-infrared imaging that will also be performed on NEAR. Unlike the
imager, the NLR does not rely on solar illumination and can make
measurements over the entire asteroid surface, including the dark
side. The NLR and the NEAR multispectral imager are boresighted, and
the imager can detect the laser spot when NLR is operated in its 8-Hz
mode over the dark side of the asteroid. Laser altimetry further
complements imaging because the direct range measurements enable
unambiguous determinations of topography that will improve the
interpretation of images.
Laser altimetry will shed new light on geological processes on the
surfaces of small bodies by allowing study of surface features such as
craters, as well as grooves and vents if present.
NLR Description
The Near Laser Rangefinder is an incoherent, direct-detection laser
altimeter. It is designed for high probability of detection in
single-pulse operation out to beyond a 50-km range for low albedo,
diffusely reflecting surfaces. The instrument uses leading-edge
detection with commandable thresholds and range gates, but does not
perform waveform analysis.
The NLR is the first spaceborne laser altimeter to have continuous
inflight range calibration capability. This is implemented with an
optical fiber delay coil of known length, through which a small
fraction of every emitted laser pulse is sent. The time at which the
light from the calibration coil is detected after each shot then
serves to calibrate the timing circuit end-to-end.
Science Objectives
- Yield rapid, accurate asteroid shape determinations
- Measure detailed surface morphology to study geological processes
- Make a vital contribution to the overall science return from NEAR
NLR Management
- Science Team Leader:
- Maria Zuber (MIT, NASA GSFC)
- Lead Engineer:
- Timothy D. Cole (JHU/APL)
- Instrument Scientist:
- Andrew F. Cheng (JHU/APL)
- NEAR Payload Manager:
- Robert E. Gold (JHU/APL)
Links to the other NEAR instruments:
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