Key Products

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BR3.2F

Our flagship product is the Bigger Rocket version 3.2 [Fixed]. The BR3.2F is a heavy-lift rocket designed for maximum cost savings to open up spaceflight to a wider market. Key to its design philosophy is Bootstrap Principle #1- no corner spared! This results in a launch system with almost the same performance as its competitors at a fraction of the cost!
This page will detail the design and performance of the BR3.2F as well as compare it to its primary competitors.

BR1.jpg
The BR3.2F in the Vehicle Assembly Building (VAB)

Overall Metrics

Height: 31.49m
Width: 6.66m
Empty mass: 47.60 tonnes
Loaded mass: 245.05 tonnes
Payload to Low Earth Orbit (LEO): 27 tonnes

Comparison with Competitors

Comparison
Metric
BR3.2F
Falcon 9
Delta IV
Height
31.49m
69.8m
70.7m
Empty Mass
47.60 tonnes
29.5 tonnes
29.5 tonnes
Loaded Mass
245.05 tonnes
549 tonnes
249.5 tonnes
Number of Stages
4
2
2
Total Number of Engines
15
10
2
Payload to LEO
27 tonnes
22.8 tonnes
25.3 tonnes
Launch Success Rate
28/47- 59.6%
439/442- 99.3%
44/45- 97.8%
Cost per Launch
563,000 USD
69.75 million USD
164 million USD
There are no rows in this table
At less than 1% the cost of our competitors while providing 95% the payload capacity, the BR3.2F is truly in a class of its own. And 59.6% success rate is almost a passing grade!

Sources:
Falcon 9
Last edited: Sat, Feb 22, 2025
Falcon 9 is a partially reusable, human-rated, two-stage-to-orbit, medium-lift launch vehicle designed and manufactured in the United States by SpaceX. The first Falcon 9 launch was on 4 June 2010, and the first commercial resupply mission to the International Space Station (ISS) launched on 8 October 2012. In 2020, it became the first commercial rocket to launch humans to orbit. The Falcon 9 has an exceptional safety record, with 439 successful launches, two in-flight failures, one partial failure and one pre-flight destruction. It is the most-launched American orbital rocket in history.
The rocket has two stages. The first (booster) stage carries the second stage and payload to a predetermined speed and altitude, after which the second stage accelerates the payload to its target orbit. The booster is capable of landing vertically to facilitate reuse. This feat was first achieved on flight 20 in December 2015. As of 18 February 2025, SpaceX has successfully landed Falcon 9 boosters 395 times. Individual boosters have flown as many as 26 flights. Both stages are powered by SpaceX Merlin engines, using cryogenic liquid oxygen and rocket-grade kerosene (RP-1) as propellants.
The heaviest payloads flown to geostationary transfer orbit (GTO) were Intelsat 35e carrying 6,761 kg (14,905 lb), and Telstar 19V with 7,075 kg (15,598 lb). The former was launched into an advantageous super-synchronous transfer orbit, while the latter went into a lower-energy GTO, with an apogee well below the geostationary altitude. On 24 January 2021, Falcon 9 set a record for the most satellites launched by a single rocket, carrying 143 into orbit.
Falcon 9 is human-rated for transporting NASA astronauts to the ISS, certified for the National Security Space Launch program and the NASA Launch Services Program lists it as a "Category 3" (Low Risk) launch vehicle allowing it to launch the agency's most expensive, important, and complex missions.
Several versions of Falcon 9 have been built and flown: v1.0 flew from 2010 to 2013, v1.1 flew from 2013 to 2016, while v1.2 Full Thrust first launched in 2015, encompassing the Block 5 variant, which has been in operation since May 2018.
See more
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en.wikipedia.org
Delta IV
Last edited: Sat, Feb 1, 2025
Delta IV was a group of five expendable launch systems in the Delta rocket family. It flew 45 missions from 2002 to 2024. Originally designed by Boeing's Defense, Space and Security division for the Evolved Expendable Launch Vehicle (EELV) program, the Delta IV became a United Launch Alliance (ULA) product in 2006. The Delta IV was primarily a launch vehicle for United States Air Force (USAF) military payloads, but was also used to launch a number of United States government non-military payloads and a single commercial satellite.
The Delta IV had two main versions which allowed the family to cover a range of payload sizes and masses: the Medium (which had four configurations) and Heavy. The final flight of Medium occurred in 2019. The final flight of Heavy was in April 2024.
Delta IV vehicles were built in the ULA facility in Decatur, Alabama. Final assembly was completed at the launch site by ULA: at the horizontal integration facility for launches from SLC-37B pad at Cape Canaveral and in a similar facility for launches from SLC-6 pad at Vandenberg Space Force Base.
See more
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en.wikipedia.org

Stage 1

Purpose and Function
Stage 1 provides the majority of thrust at liftoff. Solid rockets are non-throttleable, burning at full throttle until fuel runs out. However, they are also powerful and extremely cost-effective. Once fuel is exhausted, Stage 1 is jettisoned.
Dimensions
Mass: 144.4 tonnes
Height: 16.37m
Powerplant
6x SRB-25K “Kickback” solid-rocket booster
594kN thrust each
195s specific impulse
3,564kN total
Other Features
none
Origins
The SRB-25Ks are sourced from decommissioned Soviet-era ICBMs scheduled for disposal. So far there have only been two instances of SRB-25Ks being accidentally launched with intact warheads.
Other notes
Following repeated instances of Rapid Unscheduled Disassembly (RUD), the BR3.2 underwent a series of improvements to structural integrity to prevent the SB-12Cs from detaching prematurely from the core rocket. It was determined that simply adding more struts until it worked would be cheaper than an expensive analysis to determine the optimal placement of supports. This fulfills Bootstrap Principle #2- if it works, it works!

Images:

br2.jpg
A single SRB-25K booster

Stage 1B

Purpose and Function
Stage 1B ignites concurrently with Stage 1, providing additional thrust as well as attitude control during the initial portion of flight. After Stage 1 burns out, Stage 1B continues to burn, providing sustaining thrust to the BR3.2F and boosting it into a safe suborbital trajectory.
Dimensions
Mass: 50.36 tonnes
Height: 12.27m
Powerplant
6x Mk-55 “Thud” MethaLOx engines
126kN thrust each
275s specific impulse
These engines provide the majority of thrust for the sustainer as well as attitude control thanks to their gimballed design. Unlike the solid boosters of Stage 1, MethaLOx engines are throttleable and can have their thrust adjusted or be disabled and restarted at any time during flight.
1x 48-7S “Spark” MethaLOx engine
17.1kN thrust
270s specific impulse
774.3kN thrust total
Other Features
12x aerodynamic fins for static stability
Origins
MethaLox mix is stored in repurposed commercially-available propane storage tanks. The exterior hull consists of an upcycled grain silo. Engines are purchased pre-owned from IBay.
Other notes
The 48-7S engine was only introduced in version 3.2. Previously, the tail of the stage simply featured an aerodynamic fairing, but our engineers realized that was a waste of space and “slapped an engine ‘ere” [Chief Engineer Jeb].
Rumors that these fins are made of cardboard are false- we only use the highest quality particle board for our aerodynamic surfaces!

Images:

br3.jpg
Stage 1B

Stage 2

Purpose and Function
Stage 2 ignites shortly after burnout and separation of Stage 1B. Its primary role is to boost the payload from a suborbital to an orbital trajectory, additionally providing delta-V for inclination changes and any major orbital maneuvers. It is built to an even higher quality than our other stages, featuring a professional-grade engine and purpose-built fuel/oxidizer tanks.
Dimensions
Mass: 46.47 tonnes
Height: 12.57m
Powerplant
1x RE-15M “Skipper” MethaLOx engine
525.5kN thrust
322s specific impulse
Other Features
None
Origins
A local rocket parts provider had a typo in the product listing for the stage, allowing BLS to purchase them in substantial quantities at a fraction of their value! While this has started an ongoing legal battle we must remember Bootstrap Principle #7- take any opportunity as soon as it presents itself!
Other notes
As an employee of Bootleg Launch Solutions we must remind you that you are bound by NDA to never discuss the origins of our products or their components.

Images:

br4.jpg
Stage 2

Stage 3

Purpose and Function
Stage 3 is the final stage of the BR3.2F and also includes the crew capsule. Our analysis determined that this stage had the most significant cost savings potential, particularly in the crew capsule. Such components are typically heavy, complex and expensive, all to provide a livable environment for the crew. However, the crew’s provided spacesuits offer the same protection! So, we were able to cut significant costs with our revolutionary external cockpit design- the crew will be situated in external seats, with a nuclear generator providing both power for the control systems and warmth for our brave passengers!
Dimensions
Mass: 3.57 tonnes
Height: 5.58m
Powerplant
1x LV-1000 “Kornet” MethaLOx engine
38.0kN thrust
375s specific impulse
Other Features
Control module
Communications antenna
Federally required monopropellant reaction control system
PB-NUK Radioisotope Thermoelectric Generator
Battery
Origins
Despite their visual similarity and coincidental timing, the tanks and thrusters for Stage 3 are unrelated to Apogee Space System’s missing shipment of VL-500 “Coronet”-powered Neutron boost stages.
PB-NUK RTGs sourced from warheads originally attached to SRB-25K ICBMs.
6x Walmart-brand AAA batteries
Other notes
Stage 3 lacks reentry/landing capabilities. We are Bootstrap Launch Solutions, not Bootstrap Landing Solutions after all. Remember Bootstrap Principle #10- deliver as required and nothing more!

Images:

br6.jpg
Stage 3 with aerodynamic fairing
br5.jpg
Stage 3 in orbit with a trio of happy customers!


All images Kerbal Space Program 2 screenshots
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