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Falcon Heavy | Nancy Grace Roman Space Telescope

Recorded mission coverage
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Mission brief
The flight at a glance.
The Nancy Grace Roman Space Telescope is a NASA infrared space telescope with a 2.4 m (7.9 ft) wide field of view primary mirror and two scientific instruments. The Wide-Field Instrument (WFI) is a 300.8-megapixel multi-band visible and near-infrared camera, providing a sharpness of images comparable to that achieved by the Hubble Space Telescope over a 0.28 square degree field of view, 100 times larger than imaging cameras on the Hubble. The Coronagraphic Instrument (CGI) is a high-contrast, small field of view camera and spectrometer covering visible and near-infrared wavelengths using novel starlight-suppression technology. Roman objectives include a search for extra-solar planets using gravitational microlensing, and probing the expansion history of the Universe and the growth of cosmic structure, with the goal of measuring the effects of dark energy, the consistency of general relativity, and the curvature of spacetime.
Open the full mission →Published flight sequence
Know what comes next.
Planned timings relative to the target. These steps do not indicate live progress.
- T−00:53:00
GO for Prop Load
- T−00:50:00
Stage 1 Propellant Load
- T−00:45:00
Stage 1 LOX Load
- T−00:35:00
Stage 2 Propellant Load
- T−00:18:30
Stage 2 LOX Load
- T−00:07:00
Engine Chill
See all 29 published steps ↓
- T−00:00:59
Startup
- T−00:00:45
GO for Launch
- T−00:00:20
Tank Press
- T−00:00:06
Ignition
- T+00:00:00
Liftoff
- T+00:01:08
Max-Q
- T+00:02:24
SBECO
- T+00:02:27
Boosters Separation
- T+00:02:32
Boosters Flip
- T+00:02:43
Boosters Boostback Burn Startup
- T+00:03:48
Boosters Boostback Burn Shutdown
- T+00:03:51
MECO
- T+00:03:54
Stage 2 Separation
- T+00:04:00
SES-1
- T+00:04:15
Fairing Separation
- T+00:06:19
Boosters Entry Burn Startup
- T+00:06:29
Boosters Entry Burn Shutdown
- T+00:07:23
Boosters Landing Burn
- T+00:07:40
Boosters Landing
- T+00:08:28
SECO-1
- T+00:24:33
SES-2
- T+00:26:32
SECO-2
- T+00:31:31
Payload Separation
