national aeronautics and space administration sounding rockets

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0 40 80 120 160 200 240 280 320 100 600 500 400 300 200 Sounding Rockets Payload 2nd stage rocket motor 1st stage rocket motor National Aeronautics and Space Administration Sounding rockets carry experiments to altitudes between 50 and 1,500 km and fly nearly parabolic trajectories. Science missions, such as studies of the Earth’s near space environment, solar physics, planetary investigations and astrophysics are flown using sounding rockets. To enable scientists to study geographi- cally unique phenomena, such as the Aurora Borealis or southern sky astrophysics, launch sites around the globe are used. Sounding rockets also enable quick turn around development and testing of new science instruments and technologies for future space missions. A recovery system, such as a parachute for land impact, combined with a bouyant section for water impact, can be added to facilitate recovery and re-use of the payload. Payload Systems (telescope payload) Vehicle Configurations Sample Trajectory Terrier First stage Black Brant Second stage Payload support systems include recovery systems, telemetry, boost guidance systems, Attitude Control Systems, deployment mechanisms, and a shutter door among others. Mission requirements determine which support systems are used. Payload www.nasa.gov Puerto Rico Brazil Hawaii Marshall Islands Norway (Svalbard site) Norway Sweden Australia NASA Wallops Flight Facility Home of Sounding Rockets Alaska New Mexico Peru Greenland Active Launch Sites Inactive Launch Sites Geospace Science Solar Physics Astrophysics Technology Development Solar System Exploration Reimbursable Missions Student Outreach Geospace Science Solar Physics Astrophysics Reimbursable Student outreach Technology Development Microgravity Solar System Exploration 14% 10% 43% 7% 2% 8% 12% 3% HIGHLIGHTS Black Brant V Terrier Terrier Terrier Talos 0 5 10 15 20 55 50 45 40 35 30 25 65 60 0 5 10 15 20 Terrier Terrier Improved Orion Malemute Black Brant Black Brant Black Brant Black Brant Nihka Nihka Talos Terrier Terrier Improved Malemute Improved Orion 21 29 52 51 46 41 36 35 30 Black Brant X Black Brant IX Black Brant XI-A Black Brant XII-A Parachute Recovery The Ogive Recovery System Assembly (ORSA) houses the parachute and deployment mechanism. Boost Guidance The S19 is a boost guidance system that keeps the vehicle on a pre-programmed track for the early portion of the flight. Telemetry The Telemetry system enables experiment data to be transmitted to a ground station. Experiment This section houses the scientific instruments. Shutter Door Used mainly for telescope payloads, the shutter door is opened in space allowing the telescope to see the target of investigation. This trajectory profile, for a two stage Black Brant IX sounding rocket carrying a solar telescope payload, shows altitude in kilometers vs. time in seconds. When the fuel in each stage of the vehicle is expended the empty casing is dropped from the stack and the next stage is ignited. As the payload reaches the desired altitude, the ASC aligns the instrument with the science target, in this example the Sun, and data collection starts. The data is transmitted to a ground station and recorded for later analysis by the researchers. All parts re-enter the atmosphere and land downrange from the launch site. Some payloads are equipped with parachutes and are recovered and reused. ACS Attitude Control Systems (ACS) are used to align the payload in space. Sounding rocket launch data from 1993 through 2016 as percentage of the science and technology disciplines. A total of 495 launches were conducted during this time period. Support of the International Geophysical Year (IGY) 1957 included 210 sounding rocket launches Multiple-payloads reveal temporal-spatial scales within Aurora, Alfvén Waves, Electrostatic Structures Direct measurements in the Earth’s cusp region from Spitzbergen NASA’s first “tailored” trajectory reveals vertical, horizontal winds over Auroral arc Direct penetration of lightning electric fields�in the Ionosphere - high telemetry rates reveal new Wave Physics Highest resolution EUV images reveal how braided magnetic fields heat solar corona • Highest resolution observations of the Sun in the 52-63 nm range Underflight calibration of solar observing satellites Studies of the Sun’s effects on planetary atmospheres and the heliosphere Investigation of the cause of solar flares Imagery of nanoflares on the Sun and their impact on coronal heating Search for signatures of first light in the Extragalactic Background • Study diffuse X-rays of the Local Galaxy • Spectral studies of the Interstellar Medium (ISM) to assess the availability of star and planet forming raw materials Soft X-ray spectroscopy of Supernovae Highest Mach number inlfatable test conducted with Inflatable Re-entry Vehicle (IRVE) Mars lander parachute concept testing Strongest ever carbon monoxide production discovered in coma of Comet Hale-Bopp Study the history of water on Venus and its escape from the planet’s atmosphere • Composition of Comet ISON measured Launches to research Comet Shoemaker-Levy impact on planet Jupiter Studies of ionospheric conditions and the impact on radio and satellite communica- tions Specialty vehicle development for Department of Defense Students participate in sounding rocket missions through science missions as undergraduate and graduate students Dedicated missions for experiments provided by University students and faculty are flown on Terrier-Orion and Terrier-Improved Malemute vehicles Altitude (km) Time (sec)

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Page 1: National Aeronautics and Space Administration Sounding Rockets

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Sounding Rockets

Payload 2nd stagerocket motor

1st stagerocket motor

National Aeronautics and Space Administration

Sounding rockets carry experiments to altitudes between 50 and 1,500 km and fly nearly parabolic trajectories. Science missions, such as studies of the Earth’s near space environment, solar physics, planetary investigations and astrophysics are flown using sounding rockets. To enable scientists to study geographi-cally unique phenomena, such as the Aurora Borealis or southern sky astrophysics, launch sites around the globe are used. Sounding rockets also enable quick turn around development and testing of new science instruments and technologies for future space missions. A recovery system, such as a parachute for land impact, combined with a bouyant section for water impact, can be added to facilitate recovery and re-use of the payload.

Payload Systems (telescope payload)

Vehicle Configurations Sample Trajectory

Terr

ier

Firs

t sta

geBl

ack

Bran

tSe

cond

sta

ge

Payload support systems include recovery systems, telemetry, boost guidance systems, Attitude Control Systems, deployment mechanisms, and a shutter door among others. Mission requirements determine which support systems are used.

Payl

oad

www.nasa.gov

Puerto Rico

Brazil

Hawaii

Marshall Islands

Norway (Svalbard site)

Norway Sweden

Australia

NASA Wallops Flight FacilityHome of Sounding Rockets

Alaska

New Mexico

Peru

Greenland

Active Launch SitesInactive Launch Sites

Geospace Science

Solar Physics

Astrophysics

Technology Development

Solar System Exploration

Reimbursable Missions

Student Outreach

Geospace Science

Solar Physics

AstrophysicsReimbursable

Student outreach

Technology Development

Microgravity

Solar SystemExploration

14%

10%

43%

7%

2%

8%

12%

3%

HIGHLIGHTS

Blac

k Br

ant V

Terr

ier

Terr

ier

Terr

ier

Talo

s

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Terr

ier

Terr

ier

Impr

oved

Ori

onMal

emut

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Blac

k Br

ant

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k Br

ant

Blac

k Br

ant

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k Br

ant

Nih

ka

Nih

ka

Talo

s

Terr

ier

Terr

ier

Impr

oved

Mal

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oved

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Black Brant XBlack Brant IX

Black Brant XI-A

Black Brant XII-A

Parachute Recovery The Ogive Recovery System Assembly (ORSA) houses the parachute and deployment mechanism.

Boost Guidance The S19 is a boost guidance system that keeps the vehicle on a pre-programmed track for the early portion of the flight.

Telemetry The Telemetry system enables experiment data to be transmitted to a ground station.

ExperimentThis section houses the scientific instruments.

Shutter DoorUsed mainly for telescope payloads, the shutter door is opened in space allowing the telescope to see the target of investigation.

This trajectory profile, for a two stage Black Brant IX sounding rocket carrying a solar telescope payload, shows altitude in kilometers vs. time in seconds. When the fuel in each stage of the vehicle is expended the empty casing is dropped from the stack and the next stage is ignited. As the payload reaches the desired altitude, the ASC aligns the instrument with the science target, in this example the Sun, and data collection starts. The data is transmitted to a ground station and recorded for later analysis by the researchers. All parts re-enter the atmosphere and land downrange from the launch site. Some payloads are equipped with parachutes and are recovered and reused.

ACS Attitude Control Systems (ACS) are used to align the payload in space.

Sounding rocket launch data from 1993 through 2016 as percentage of the science and technology disciplines. A total of 495 launches were conducted during this time period.

Support of the International Geophysical Year (IGY) 1957 included 210 sounding rocket launches • Multiple-payloads reveal temporal-spatial scales within Aurora, Alfvén Waves, Electrostatic Structures • Direct measurements in the Earth’s cusp region from Spitzbergen • NASA’s first “tailored” trajectory reveals vertical, horizontal winds over Auroral arc • Direct penetration of lightning electric fields�in the Ionosphere - high telemetry rates reveal new Wave Physics

Highest resolution EUV images reveal how braided magnetic fields heat solar corona • Highest resolution observations of the Sun in the 52-63 nm range • Underflight calibration of solar observing satellites • Studies of the Sun’s effects on planetary atmospheres and the heliosphere • Investigation of the cause of solar flares • Imagery of nanoflares on the Sun and their impact on coronal heating

Search for signatures of first light in the Extragalactic Background • Study diffuse X-rays of the Local Galaxy • Spectral studies of the Interstellar Medium (ISM) to assess the availability of star and planet forming raw materials • Soft X-ray spectroscopy of Supernovae

Highest Mach number inlfatable test conducted with Inflatable Re-entry Vehicle (IRVE) • Mars lander parachute concept testing

Strongest ever carbon monoxide production discovered in coma of Comet Hale-Bopp • Study the history of water on Venus and its escape from the planet’s atmosphere • Composition of Comet ISON measured • Launches to research Comet Shoemaker-Levy impact on planet Jupiter

Studies of ionospheric conditions and the impact on radio and satellite communica-tions • Specialty vehicle development for Department of Defense

Students participate in sounding rocket missions through science missions as undergraduate and graduate students • Dedicated missions for experiments provided by University students and faculty are flown on Terrier-Orion and Terrier-Improved Malemute vehicles

Altit

ude

(km

)

Time (sec)