Hera (space mission)

  Hera ·  Sun ·  65803 Didymos ·  Mars ·  Earth

Deimos over Terra Sabaea, photo taken by Hera on 12 March 2025, processed by Andrea Luck.

Launch

Hera launched on 7 October 2024 at 14:52 UTC by a Falcon 9 rocket lifting off from Space Launch Complex 40 (SLC-40) at Cape Canaveral Space Force Station. ^[27] Usually, Falcon 9 launches for beyond geostationary transfer orbit are made from the nearby Launch Complex 39A (LC-39A) at Kennedy Space Center due to SLC-40's focus on Starlink launches. However, LC-39A was in the midst of preparing for the launch of NASA's Europa Clipper on a Falcon Heavy later in the week, which locked Hera into using SLC-40. Additionally, the launch occurred while Falcon 9 was grounded due to a mishap with a second stage deorbit burn happening the SpaceX Crew-9 mission the previous month. As Hera was to be put into a heliocentric orbit however, FAA waived the grounding for its launch as an exception. The booster used for the launch was expended to help with the trajectory; it previously flew 22 times, including on missions like SpaceX Crew-1 and the IXPE. ^{[28] [29]}

Cruise towards Mars

On 10 and 11 October 2024, Hera tested three of its science instruments (AFC, TIRI, and HyperScout H) by using them to take pictures of Earth and the Moon from a distance of more than one million km. ^[30]

In October 2024, the two CubeSats aboard Hera were briefly activated to confirm their nominal status and test their ability to communicate with Earth. This marked the first operation of CubeSats in deep space by ESA. ^[31]

Following three successful test burns performed after launch, the spacecraft conducted its first deep-space maneuver on 27 October 2024, firing its three orbital control thrusters for 100 minutes and changing its velocity by ~146 m/s, and second on 6 November 2024, firing for 13 minutes and changing its velocity by ~20 m/s. ^[32]

Mars flyby

Hera performed a gravity assist at Mars on 12 March 2025, coming at a distance of 5,000 km (3,100 mi) from the surface. As part of the flyby, the spacecraft spent some time observing the Martian moon Deimos, imaging it from distance of 1,000 km (620 mi) and having its closest approach at 300 km (190 mi) away. ^[33] During the flyby, Hera also autonomously locked onto impact craters and other surface features on Mars to track them over time, in a full-scale test of the autonomous navigation techniques it will use to navigate around its targets. ^[34]

Cruise through the main asteroid belt

On 11 May 2025, the mission has captured images of the asteroid (1126) Otero from a distance of approximately 3 million km and on 19 July 2025 of the asteroid (18805) Kellyday from a distance of approximately 6 million km in order to perform instrument tests and to demonstrate agile spacecraft operations useful for planetary defence. ^[35]

Arrival at Didymos

The spacecraft will reach the binary asteroid (65803) Didymos on 28 December 2026, four years after DART, to begin six months of investigation. Hera will be the first to make a rendezvous with a binary asteroid. Once close to the double asteroid, five stages will follow:

Hera

Artist's impression of Hera in orbit around the asteroid Didymos
Mission type	Didymos orbiter
Operator	European Space Agency
COSPAR ID	2024-180A
SATCAT no.	61449
Website	heramission.space
Mission duration	10 months, 30 days (elapsed) 2 years, 9 months (planned) [a]
Spacecraft properties
Manufacturer	OHB SE
Launch mass	1,128 kg (2,487 lb)
Dry mass	350 kg (770 lb)
Dimensions	1.6 × 1.6 × 1.7 m (5.2 × 5.2 × 5.6 ft)
Start of mission
Launch date	7 October 2024, 14:52:11  UTC [1] [2] (10:52:11 am  EDT)
Rocket	Falcon 9 Block 5 B1061-23
Launch site	Cape Canaveral, SLC‑40
Contractor	SpaceX
Flyby of Deimos
Closest approach	12 March 2025, 12:07  GMT
Distance	300 km (190 mi)

Mission phases ^[36]

Phase	Mission phase	Duration	Mission
1	Early Characterization	6 weeks	The global shape and mass/gravity, as well as thermal and dynamical properties, of both asteroids will be determined
2	Payload Deployment	2 weeks	The release of the two CubeSats
3	Detailed Characterization	4 weeks	Meter-scale mapping of the asteroids and determination of thermal, spectral, and interior properties
4	Close Observation	6 weeks	High-resolution investigations of a large fraction of the surface area of Dimorphos, including the DART impact crater
5	Experimental	6 weeks	Morphological, spectral, and thermal properties of Dimorphos

Spacecraft

The main bus of Hera has a box-shape based on a central tube and adapter cone of 1.6 × 1.6 × 1.7 meters. Two solar panel wings extend from opposite sides, and a high-gain dish antenna is mounted on one face. Total launch mass of the spacecraft is approximately 1214 kg, the dry mass is 696 kg. Spacecraft deployed dimensions are 2.2 x 11.4 x 2.2 meters. The solar panels have an area of about 13 square meters. The spacecraft will use 712 W at the nominal 2.4 AU distance. Bi-propellant chemical propulsion is used for 16 orbit control thrusters and 6 reaction control thrusters, all 10-N motors. Total available delta-V is about 1300 m/s. Communications with the ground are X-band (~8.4 GHz), with two low gain antennas in addition to the high-gain dish. S-band communications (~2.2 GHz), using patch antennas, will be used to communicate with the two CubeSats named Juventas and Milani, with a range of 60 km. Spacecraft orientation is maintained by 4 reaction wheels, gyroscopes, using star trackers and solar sensors, as well two Asteroid Framing Cameras (AFC). Attitude guidance is through the Planetary Altimeter (PALT). ^{[37] [38] [39]}

Scientific instruments

Asteroid framing cameras (AFC)

The main instruments of Hera are the two AFC cameras (Asteroid Framing Cameras), developed by the company JenaOptronik. Identical and redundant, they each have a FaintStar panchromatic sensor of 1020 x 1020 pixels with a telephoto lens. The field of view is 5.5 x 5.5 degrees, and the spatial resolution reaches one meter at a distance of 10 kilometers. These cameras are to provide physical characteristics of the surface of the asteroid Didymos and Dimorphos as well as the crater created by DART and the Juventas landing zone.^{[ citation needed ]}

Hyperspectral imager – HyperScout-H

HyperScout-H is a hyperspectral imager that must provide images in a spectral range between 665 and 975 nm (visible and near infrared). The instrument makes its observations in 25 distinct spectral bands. It is developed by cosine Remote Sensing. This is a specific version developed for Hera, different from the standard HyperScout.^{[ citation needed ]}

Planetary altimeter (PALT)

PALT is a micro-Lidar planetary altimeter using a laser emitting an infrared light beam at 1.5 microns. Its track on the ground is 1 meter at an altitude of 1 kilometer (1 milliradian). The altitude measurement accuracy is 0.5 meters. Its frequency is 10 Hertz.^{[ citation needed ]}

Thermal Infrared Imager (TIRI)

TIRI is a thermal infrared imager provided by the JAXA, the Japanese space agency. The spectral range observed is between 7 and 14 microns and it has 6 filters. Its visual range is 13.3 x 10.6°. The spatial resolution is 2.3 meters at a distance of 10 kilometers.^{[ citation needed ]}

X-Band Radio Science (X-DST)

The mass of the two asteroids making up the binary system, the characteristics of their gravity field, their rotational speed, and their orbits will be measured using radio wave disturbances caused by the Doppler effect. The measurements relate to the radio exchanges between Hera and Earth stations but also between Hera and the CubeSats. Due to the low orbit in which the CubeSats will circulate, these last measurements are crucial to determine the gravity of Didymos.^{[ citation needed ]}

Main characteristics of the instruments

	AFC	HyperScout-H	PALT	TIRI
Type	Visible Imager	Spectral imager	Altimeter	Thermal infrared imager
Mass (kg)	<1.5	5.5	4.5	<4.4
Visual range (degrees)	5.5	15.5 x 8.3	non-applicable	13.3 x 10
Spatial resolution (microradians)	94.1	133	1000	226
Spectral band (nanometers)	350-1000	665-975		700-1400
Others		25 spectral bands	vertical precision : 0.5 m.	6 filters
Power (Watts)	<1.3	2.5 (average) - 4.5 (peak)	<14.5	20 (average) - <30

CubeSats

Two CubeSat type nanosatellites, named Milani and Juventas, are transported by Hera and released before arrival in the asteroidal system (65803) Didymos. They are responsible for carrying out investigations that complement those of their carrier ship. Both CubeSats are built around a similar platform. These are 6U-XL CubeSats with a mass (including propellant) of approximately 12 kilograms. They are 3-axis stabilized and have a cold gas propulsion system. They communicate with the mothership in S-band. The Doppler effect affected radio link is used to measure the characteristics of the gravitational field of the binary system. They have a visible light camera and star trackers which are used to determine the dynamic variations of Didymos. Finally, the two CubeSats are equipped with accelerometers which will be used to determine the properties of the surface of Dimorphos if the CubeSats land on its surface as planned at the end of their mission. Juventas was developed by GomSpace and Milani by Tyvak International.^{[ citation needed ]}

Juventas

The CubeSat Juventas aims to determine the geophysical characteristics of Dimorphos. The probe will map its gravity field and determine its internal structure as well as the characteristics of its surface.

To fulfill these objectives, it carries the following instruments:

• The JuRa radar operating in the 50–70 MHz frequency with a spatial resolution of 10 to 15 meters. It is the first instrument to probe the inner layers of an asteroid. It uses two dipole antennas with each branch measuring 1.5 meters. Each measurement session can last up to 45 minutes. It occupies a volume of less than 1U and its mass is less than 1300 grams.
• The GRASS gravimeter whose dynamic range is 5 x 10⁻⁴ and sensitivity is 5 x 10⁻⁷. Its mass is less than 380 grams.
• A camera.
• The radio link with the mother ship (measurement of the Doppler effect).^{[ citation needed ]}

Milani

The CubeSat Milani (named after Andrea Milani) aims to take images and measure the characteristics of the possibly present dust. It will map the two asteroids forming the binary asteroid 65803 Didymos, characterize their surface, evaluate the effects of the DART impact, contribute to the measurements of the gravitational field of the asteroids, and determine the characteristics of the dust clouds possibly located around the asteroids.

To fulfill these objectives, it carries two instruments:

• The ASPECT hyperspectral imaging spectrometer is the main instrument. It works in visible and near infrared light (0.5 to 2.5 microns). Its spatial resolution is 2 meters at 10 kilometers and its spectral resolution is less than 40 nanometers (20 nanometers in the visible). It has a total of 72 channels.
• The VISTA thermogravimeter is responsible for detecting dust (5 to 10 microns), volatiles (such as water) and light organic materials.^{[ citation needed ]}

See also

• Near-Earth Object Coordination Centre (ESA's NEOCC)
• Planetary Defense Coordination Office (NASA's PDCO)
• Double Asteroid Redirection Test (DART mission)
• List of European Space Agency programmes and missions

Notes

1. 2 year, 3 month cruise phase, followed by a 6 month science phase

References

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Bibliography

• Michel, Patrick; Cheng, A.; Küppers, M.; Pravec, P.; Blum, J.; Delbo, M.; Green, S.F.; Rosenblatt, P.; Tsiganis, K.; Vincent, J.B.; Biele, J.; Ciarletti, V.; Hérique, A.; Ulamec, S.; Carnelli, I.; Galvez, A.; Benner, L.; Naidu, S.P.; Barnouin, O.S.; Richardson, D.C.; Rivkin, A.; Scheirich, P.; Moskovitz, N.; Thirouin, A.; Schwartz, S.R.; Campo Bagatin, A.; Yu, Y. (June 2016). "Science case for the Asteroid Impact Mission (AIM): A component of the Asteroid Impact & Deflection Assessment (AIDA) mission" (PDF). Advances in Space Research. 57 (12): 2529–2547. Bibcode:2016AdSpR..57.2529M. doi:10.1016/j.asr.2016.03.031. S2CID   42465954.
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External links

• Hera mission by Côte d'Azur Observatory
• Hera mission by European Space Agency
• Hera and Planetary Defense, COSPAR 2021, P. Michel, 4 February 2021.
• Science return of Hera, COSPAR 2021, P. Michel, 2 February 2021.
• Youtube channel of the NEO-MAPP project.
• The Planetary Science Journal, volume 3, number 7, 2022, July, 15th.