Instruments

 
Ramses_mission_concept.jpg

TIRI

Thermal Infra Red Imager

TIRI is a contribution by ISAS and the JAXA (Japan eXploration Agency), manufactured by MEC. Investigation of thermo-physical properties of Apophis, especially thermal inertia, and distribution of materials.

 

Parameters

 Detector  Lyndred PICO1024 Gen2

Wavelength

 7-14μm

 

 Number if pixels  1024(H) x 768 (V)
 Pixel size  17μm
 Detection area size

17.5 x 13.1mm

 Absolute temp accuracy  ~3K
 Temperature range

150 ~ 450K

Field of view (FOV)

13.3x10.0

Angular Resolution (IFOV)

 0.023 mrad (0.013°/pixel)

Main body size

 150 x 180 x 230mm
 Mass  4.2 kg ≤ 5.5 kg (with system margin)
 

Hamlet

Hyperspectral Imager

Based on Hera Hyperscout-H, Observing in 45 visible and near-infrared spectral bands, the HyperScout hyperspectral imager is developed by Cosine Research and INAF IAP in Italy and will contribute to the geological and compositional investigation of the asteroid. It will facilitate the identification and quantification of silicate minerals (modal abundances of olivine, orthopyroxene, & clinopyroxene, their Fe, Mg, and Ca content).

 

Parameters (NIR Channel)

 Field of View  15.97°x9.85°
 Focal Length  41.25mm

Pixel Pitch

 5.5μm
 Spectral Range  650-960nm

Parameters (SWIR Channel)

 Field of View  8.8°x7°
 Focal Length  42.308mm

Pixel Size

 5μm
 Spectral Range  950-1500nm

CHANCES
Colour High-resolution Apophis Narrow-angle CamEra System 

Multispectral Imager

A Comet-I CoCa adaptation from Uni Bern (CH) and LAM (FR). Vis-NIR multispectral imaging system (~400 to ~1700 nm). High resolution images, i.e., ~1.5 cm at closest approach - covering the part of the near-Infrared spectrum and including the 1-μm absorption band and reflectance maximum at 1.6 μm for the unambiguous determination of the asteroid’s class and its possible change as it passes through Earth’s gravity field.

 

Parameters

 Telescope  Maksutov
 Detector  3D Plus, 3DCM830-1 SWIR Space Camera Head

Main Structure

 Monolithic made of AIBeMet
 E-Box  2 PCBs: DPU and DCC+FTC

DPU

 CaSSIS/CoCa heritage

Mass Budget

 3kg (including maturity margin)
 Envelope  220 x 200 x 300mm³

PALT-H
Planetary ALTimeter

Hera Rebuilt, Dual use as GNC sensor.

The Planetary ALTimeter (PALT) is a LIDAR experiment that determines the distance to the asteroids by measuring the time of flight of a laser beam at 1.5 μm wavelength with a footprint of 1 mrad (i.e. the diameter of the footprint is 10m at a distance of 10 km). The accuracy of the distance measurement is 0.5 m, the laser wavelength of 1.535 μm

PALT supports spacecraft navigation, from fly-by to landing operations, and provide scientific data, such as relative velocity, falling velocity and reflectance measurements at laser wavelength. It can support the development of the asteroid shape model and mass measurement (which allows an estimate of the bulk density) as well as the determination of the surface topography.

 

Parameters

 Laser pulse energy  100 μJ
 Pulse width  2ns

Emitter Optic Transmission

 .96

Receiver optics transmission

 .93
 Receiver telescope entrance aperture area.  70 mm
 Laser wavelength  1535 nm
 Working distance  100m to 14 km

Accuracy of distance measurement

 < 50 cm
 Footprint  1 mrad (1m from 1 km distance)
 Optical Unit with baffle plus Electronics Box  2.5 Kg

RPS
Ramses Plasma Spectrometer

RPS is a German contribution (supported by DLR) that will provide the first-ever detailed in-situ measurements of an asteroid’s plasma environment, offering key insights into its surface composition and weathering, plasma wake formation, and fundamental space plasma physics at kinetic scales.

 

Parameters

 Energy Range  1 eV/e - 60 keV/e (ΔE/E < 10%)
 Time Resolution  Adjustable, Best: 4.5 s

Angular Coverage

 360° azimuth, up to 78° polar

Angular Resolution

 22.5° azimuth, <10° polar
 Species Detection  Electrons, Ions, Negative Ions
 Instrument Status  Sensor & electronics fully developed/calibrated (in storage)

Radio Science

The Ramses radio science experiment (RSE) will contribute to the determination of the binary system’s mass, gravity field and rotational state and orbits, through processing of Doppler and ranging measurements, as well as optical images. The experiment includes classical ground-based radiometric measurements between RAMSES and ground stations on Earth by means of a standard two-way X-band link, images of Apophis taken by the on-board camera(s), and satellite-to-satellite radiometric tracking between RAMSES and the Cubesats. The latter measurement, the so-called Inter-satellite link (ISL), represents a crucial add-on to the gravity estimation of low-gravity bodies by exploiting the proximity of the Cubesats to the asteroid, as the range-rate measurements carried out by the inter-satellite link contain important information.

Cebreros_station_pillars.jpg
Hera High Gain Antenna

RAMSES High Gain Antenna