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Our Blue Ring Pathfinder hit all our mission objectives within the planned six-hour journey after being inserted into the desired orbit by New Glenn with an apogee of 19,300 km and a perigee of 2,400 km at a 30-degree inclination. GS2 and the BE-3U engines nailed insertion with a... show more

Dave Limp

32,783 subscribers

151,270 views • 1 year ago •via X (Twitter)

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11 Comments

Eric Berger1 year ago

@SpaceJosh That’s incredibly impressive on your debut orbital launch. Congratulations Dave.

FCA2 years ago

Where do you even begin? We ENGAGE, EQUIP, and EMPOWER in that order. Our E3 training provides you with tangible steps to start making disciples. We challenge you to start your discipleship journey today. We are here to help.

Kevin Chen1 year ago

Amazing news, Dave! When do you think the next launch of New Glenn will be?

Fancy Cat1 year ago

Thank you $CHAD

Booster 111 year ago

Can we pretty please see inside fairing cam for fairing jettison pleaseee 🥺

S.E. Robinson, Jr.1 year ago

Post video of Fairing separation, or it didn't happen... 😉

Jason Horton1 year ago

1% deviation is pretty good.

Lane Breckenridge1 year ago

Congratulations!!! Look forward to the next launch!

Argonautas del Espacio1 year ago

Thank you, for use metric units.

A. Pettit1 year ago

Fantastic news!

Lee Chr🅰️ska1 year ago

@spacanpanman Congratulations!!

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Last month, our Blue Ring Pathfinder launched on New Glenn, hitting all mission objectives. The second stage and the BE-3U engines reached insertion with less than 1% deviation from our exact orbital injection target. Designed for multi-mission, multi-orbit mobility, Blue Ring is redefining space maneuverability and operations.

Last month, our Blue Ring Pathfinder launched on New Glenn, hitting all mission objectives. The second stage and the BE-3U engines reached insertion with less than 1% deviation from our exact orbital injection target. Designed for multi-mission, multi-orbit mobility, Blue Ring is redefining space maneuverability and operations.

Blue Origin

122,476 views • 1 year ago

January’s GS2 performed remarkably during our inaugural New Glenn launch, delivering our payload to orbit with less than 1% deviation from the target. Today, we completed a full duration 15-second hotfire test of the upper stage for our NG-2 mission. This time, we achieved enhanced performance from the BE-3U engine, increasing the maximum thrust from 173,000 lbf to 175,000 lbf per engine, further expanding New Glenn’s capabilities for our customers.

January’s GS2 performed remarkably during our inaugural New Glenn launch, delivering our payload to orbit with less than 1% deviation from the target. Today, we completed a full duration 15-second hotfire test of the upper stage for our NG-2 mission. This time, we achieved enhanced performance from the BE-3U engine, increasing the maximum thrust from 173,000 lbf to 175,000 lbf per engine, further expanding New Glenn’s capabilities for our customers.

Dave Limp

246,460 views • 1 year ago

Polaris Dawn Dragon spacecraft achieved its nominal orbit, with an apogee height of 1,400 km and a quite low perigee of 200 km – The orbit period is around 100 minutes at an inclination of 51.7 degrees. Polaris Dawn will break several records, as SpaceX wants to fly a manned mission through the Van Allen belt, perform the first-ever commercial extravehicular activity (EVA), and a laser satellite-to-spacecraft link with Starlink.

Polaris Dawn Dragon spacecraft achieved its nominal orbit, with an apogee height of 1,400 km and a quite low perigee of 200 km – The orbit period is around 100 minutes at an inclination of 51.7 degrees. Polaris Dawn will break several records, as SpaceX wants to fly a manned mission through the Van Allen belt, perform the first-ever commercial extravehicular activity (EVA), and a laser satellite-to-spacecraft link with Starlink.

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17,197 views • 1 year ago

#WATCH | Andhra Pradesh: India's first privately developed orbital-class rocket, Vikram-1, launched from the Satish Dhawan Space Centre in Sriharikota Built by Hyderabad-based Skyroot Aerospace, Vikram-1 is powered by three solid-fuel stages and a liquid orbital adjustment module. The mission is designed to deploy payloads weighing up to 350 kg into a 450-km Low Earth Orbit (LEO) with a 60-degree inclination. (Source: Skyroot Aerospace)

#WATCH | Andhra Pradesh: India's first privately developed orbital-class rocket, Vikram-1, launched from the Satish Dhawan Space Centre in Sriharikota Built by Hyderabad-based Skyroot Aerospace, Vikram-1 is powered by three solid-fuel stages and a liquid orbital adjustment module. The mission is designed to deploy payloads weighing up to 350 kg into a 450-km Low Earth Orbit (LEO) with a 60-degree inclination. (Source: Skyroot Aerospace)

ANI

102,115 views • 9 days ago

#WATCH | Andhra Pradesh: Visuals from the Satish Dhawan Space Centre in Sriharikota; India's first privately developed orbital-class rocket, Vikram-1, will be launched from here shortly Built by Hyderabad-based Skyroot Aerospace, Vikram-1 is powered by three solid-fuel stages and a liquid orbital adjustment module. The mission is designed to deploy payloads weighing up to 350 kg into a 450-km Low Earth Orbit (LEO) with a 60-degree inclination. (Source: Skyroot Aerospace)

#WATCH | Andhra Pradesh: Visuals from the Satish Dhawan Space Centre in Sriharikota; India's first privately developed orbital-class rocket, Vikram-1, will be launched from here shortly Built by Hyderabad-based Skyroot Aerospace, Vikram-1 is powered by three solid-fuel stages and a liquid orbital adjustment module. The mission is designed to deploy payloads weighing up to 350 kg into a 450-km Low Earth Orbit (LEO) with a 60-degree inclination. (Source: Skyroot Aerospace)

ANI

60,404 views • 9 days ago

Shijian-31: a satellite with an orbit we have never seen before China launched Shijian-31 on June 16 from Xichang, officially described as a "space environment detection" mission. The orbital elements suggest more going on. The inclination 63.46° sits at the value where perigee advance goes to zero. Anyone who's tracked Molniya-class satellites will recognize that immediately. But the resemblance stops there. A classic Molniya parks its apogee over high northern latitudes and dwells for hours, that's the whole design premise. SJ-31's argument of perigee is 171°, which puts perigee near the equator and its apogee on the opposite side. (Image 1: SJ-31 at 171° argument of perigee vs. a generic Molniya at 270° argument of perigee.) So the long dwell isn't over any particular latitude — it's over altitude. Apogee reaches ~39,900 km, about 4,100 km above the operational GEO belt where comms and missile-warning satellites sit. Nearly a third of each 12.5-hour orbit is spent above that shell, crossing it twice per pass at a steep 63° angle. (Video 1: SJ-31's orbit visualized with example GEO assets.) It's also not fixed on one region. The period is just off a clean repeating ground track, so the sub-apogee point slowly drifts around the globe — sweeping past every longitude roughly once every 24 days. Net effect: an orbit that periodically looks down on the entire GEO belt from above, at an angle, on a rotating schedule, rather than fixating on one target. What's it actually doing up there? SpaceNews Breaking Defense Joey Roulette Space Domain Awareness Jonathan McDowell Integrity ISR

Shijian-31: a satellite with an orbit we have never seen before China launched Shijian-31 on June 16 from Xichang, officially described as a "space environment detection" mission. The orbital elements suggest more going on. The inclination 63.46° sits at the value where perigee advance goes to zero. Anyone who's tracked Molniya-class satellites will recognize that immediately. But the resemblance stops there. A classic Molniya parks its apogee over high northern latitudes and dwells for hours, that's the whole design premise. SJ-31's argument of perigee is 171°, which puts perigee near the equator and its apogee on the opposite side. (Image 1: SJ-31 at 171° argument of perigee vs. a generic Molniya at 270° argument of perigee.) So the long dwell isn't over any particular latitude — it's over altitude. Apogee reaches ~39,900 km, about 4,100 km above the operational GEO belt where comms and missile-warning satellites sit. Nearly a third of each 12.5-hour orbit is spent above that shell, crossing it twice per pass at a steep 63° angle. (Video 1: SJ-31's orbit visualized with example GEO assets.) It's also not fixed on one region. The period is just off a clean repeating ground track, so the sub-apogee point slowly drifts around the globe — sweeping past every longitude roughly once every 24 days. Net effect: an orbit that periodically looks down on the entire GEO belt from above, at an angle, on a rotating schedule, rather than fixating on one target. What's it actually doing up there? SpaceNews Breaking Defense Joey Roulette Space Domain Awareness Jonathan McDowell Integrity ISR

COMSPOC_OPS

285,589 views • 5 days ago

2034 Earth–Venus–Mars opportunity looks promising. 10–15 on-orbit refueling operations may be needed to make a crewed ship full. Most can be done at an altitude of 180–200 km, made possible by Starship’s size. The final refueling may be performed at a higher altitude of ~2000 km, just below the Van Allen belt. Earth departure on 2034-08-21 from 2000 km orbit. A Trans-Venus Injection burn of ~3.7 km/s will place the ship on an Earth–Venus–Earth free-return trajectory. Venus flyby is expected on 2034-12-19, 120 days after departure. Two weeks before the encounter, if the mission proceeds as planned, a 25-m/s maneuver will shift the trajectory from Earth-return to Mars-bound. If not, the ship will free return to Earth in September 2035. The Venus gravity assist will send the ship into another Earth free-return trajectory, with Mars flyby around 2035-06-02. One week before reaching Mars, a system health check will determine whether to commit to Mars Orbit Insertion. If it’s GO, a small 10-m/s manuever will put the ship to less than 100 km altitude periapsis. Otherwise, a Mars flyby will lead to an Earth return in May 2036. The ship will enter the Martian atmosphere at about 9.4 km/s, performing an aerobrake to slow to 4.88 km/s and capture into a 100x140000 km, 7-day period high elliptical orbit. At apoapsis, a 50-m/s plane change will align the inclination with Mars’ equator, followed by additional aerobraking to remove about 650 m/s of velocity, placing the spacecraft in a 120x6128 km orbit. A 550-m/s burn at 6128 km altitude will then adjust the trajectory into Phobos orbit. The ship will stay at Phobos for about 7 days. The Mars–Phobos L1 point is only about two miles above Phobos’ surface, and Mars would dominate nearly half the sky, appearing about 80 times larger than the Moon from Earth. The ship will depart for Deimos afterward. Two burns totaling roughly 750 m/s will transfer the ship from Phobos to Deimos. And the ship will stay at Deimos for 7 days more. From Deimos, the ship will raise its apoapsis to form a 20000x140000 km altitude, 7-day orbit, requiring about 420 m/s of delta-v. At apogee, a 50-m/s burn will adjust inclination and lower periapsis to ~500 km for final Trans-Earth Injection. If time and propellant allow, the orbit can be aligned to a polar inclination for Mars ice-cap observations before departure. A Trans-Earth Injection burn at 500 km altitude, requiring 1.5–1.6 km/s of delta-v in early July 2035. If departure on the first days in July, Earth arrival is expected in December 2035. If missed that window, a March 2036 arrival may look more feasible. Nominal mission duration: 490 days, with 30 days in Mars orbit and 14 days at Phobos and Deimos. Two planets, two moons for 3.7+0.025+0.010+0.05+0.42+0.55+0.75+1.55=7.06 km/s Δv

2034 Earth–Venus–Mars opportunity looks promising. 10–15 on-orbit refueling operations may be needed to make a crewed ship full. Most can be done at an altitude of 180–200 km, made possible by Starship’s size. The final refueling may be performed at a higher altitude of ~2000 km, just below the Van Allen belt. Earth departure on 2034-08-21 from 2000 km orbit. A Trans-Venus Injection burn of ~3.7 km/s will place the ship on an Earth–Venus–Earth free-return trajectory. Venus flyby is expected on 2034-12-19, 120 days after departure. Two weeks before the encounter, if the mission proceeds as planned, a 25-m/s maneuver will shift the trajectory from Earth-return to Mars-bound. If not, the ship will free return to Earth in September 2035. The Venus gravity assist will send the ship into another Earth free-return trajectory, with Mars flyby around 2035-06-02. One week before reaching Mars, a system health check will determine whether to commit to Mars Orbit Insertion. If it’s GO, a small 10-m/s manuever will put the ship to less than 100 km altitude periapsis. Otherwise, a Mars flyby will lead to an Earth return in May 2036. The ship will enter the Martian atmosphere at about 9.4 km/s, performing an aerobrake to slow to 4.88 km/s and capture into a 100x140000 km, 7-day period high elliptical orbit. At apoapsis, a 50-m/s plane change will align the inclination with Mars’ equator, followed by additional aerobraking to remove about 650 m/s of velocity, placing the spacecraft in a 120x6128 km orbit. A 550-m/s burn at 6128 km altitude will then adjust the trajectory into Phobos orbit. The ship will stay at Phobos for about 7 days. The Mars–Phobos L1 point is only about two miles above Phobos’ surface, and Mars would dominate nearly half the sky, appearing about 80 times larger than the Moon from Earth. The ship will depart for Deimos afterward. Two burns totaling roughly 750 m/s will transfer the ship from Phobos to Deimos. And the ship will stay at Deimos for 7 days more. From Deimos, the ship will raise its apoapsis to form a 20000x140000 km altitude, 7-day orbit, requiring about 420 m/s of delta-v. At apogee, a 50-m/s burn will adjust inclination and lower periapsis to ~500 km for final Trans-Earth Injection. If time and propellant allow, the orbit can be aligned to a polar inclination for Mars ice-cap observations before departure. A Trans-Earth Injection burn at 500 km altitude, requiring 1.5–1.6 km/s of delta-v in early July 2035. If departure on the first days in July, Earth arrival is expected in December 2035. If missed that window, a March 2036 arrival may look more feasible. Nominal mission duration: 490 days, with 30 days in Mars orbit and 14 days at Phobos and Deimos. Two planets, two moons for 3.7+0.025+0.010+0.05+0.42+0.55+0.75+1.55=7.06 km/s Δv

Chun

224,900 views • 9 months ago

Rocket engines are core to our mission, and we continue to increase production rates. Go behind the scenes with Michael Xu, a manufacturing process engineer whose work developing and optimizing critical welding processes for our BE-3U and BE-4 turbomachinery and tube assemblies is helping make this happen. Together, we are building a road to space for the benefit of Earth. Join Team Blue at

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Blue Origin

34,641 views • 1 year ago

.Dr Jordan B Peterson testifies before Congress and warns about the dangers of a "superstate": "Governments can and are colluding with these corporate agents to develop a picture not only of our actions but of our thoughts and words. So that deviation from the desired end can be mapped, rewarded, and punished."

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Daily Wire

224,648 views • 2 years ago

As our mission manifest grows, so have our facilities! Firefly has made improvements at our Rocket Ranch and doubled the size of our campus in Cedar Park, Texas with a new innovation lab and expansive cleanroom to enable an assembly line of lunar landers and orbital vehicles. Read more here:

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Firefly Aerospace

20,771 views • 2 months ago

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51,943 views • 2 years ago

At the culmination event of Sadhguru's 30,000-km, 100-day journey, at #IshaYogaCenter, Radhe Jaggi and Project Samskriti capture the essence of our relationship with soil and planet in a stirring dance performance. Explore more about Bharatanatyam with #ProjectSamskriti: #InternationalDanceDay #SaveSoil

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25,223 views • 3 years ago

Today, we’re taking a step toward truly galactic-scale capabilities. 🚀 We’re partnering with Sarvam to bring sovereign AI into orbit aboard India’s first orbital data centre satellite, a pathfinder mission bringing datacenter-class GPUs and high-performance remote sensing together in space. Built and operated by Pixxel, with Sarvam providing the AI backbone, the demonstrator marks a step toward making orbital data centres real, operational, and scalable from India. May the 4th be with us all! ✨

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201,088 views • 2 months ago

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Firefly Aerospace

319,025 views • 1 year ago

We just shipped a people prospecting feature that lets our users directly search through our database of 400M people records to find the exact individual they want to reach out to. Now users can research an account, use our prospector to find the exact people to target, use our deliverables feature to create an outreach message, and prepare for any meetings with the prospect with our people dossier, all within one platform. Enjoy!

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15,193 views • 2 years ago

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32,874 views • 10 months ago

The DENZA N9 completes the Fishhook Test at 180 km/h—setting a new global record. Double-certified by CCIC and China-SAE, this milestone reflects our pursuit of control, safety, and next-generation performance. Experience the future of NEVs with BYD

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Is there a “War on the Car” with new developments being approved with less and less parking and ever narrowing streets? I suggested at Council that this could be a contributing cause of increased road rage and accidents in our City.

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Dan McLean

12,163 views • 5 months ago

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All India Radio News

1,193,146 views • 3 years ago