SAILING THE PLANETS: PLANETARY EXPLORATION FROM GUIDED BALLOONS. 7 th Annual Meeting of the NASA Institute for Advanced Concepts

Similar documents
SCIENCE WITH DIRECTED AERIAL DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION SAILING THE PLANETS

Direct Aerial Robot Explorers (DARE) For Planetary Exploration

Exploring Planets with Directed Aerial Robot Explorers

Directed aerial robot explorers for planetary exploration

MARS DROP. Matthew A. Eby Mechanical Systems Department. Vehicle Systems Division/ETG The Aerospace Corporation May 25, 2013

LAB 2 HOMEWORK: ENTRY, DESCENT AND LANDING

Advanced drop tests from stratospheric balloons

SOLAR MONTGOLFIERE BALLOONS FOR MARS

Robotic Lunar Exploration Scenario JAXA Plan

MONTGOLFIERE BALLOON MISSIONS FOR MARS AND TITAN

Preface. 2 Cable space accelerator 39

Technology Reference Studies

Inflatable Robotics for Planetary Applications

Robotic Mobility Atmospheric Flight

Robotic Mobility Atmospheric Flight

Aeromaneuvering/Entry, Descent, Landing

Irvine. Salton Sea. Palm Springs. Interstate 10

Paper Session II-B - The Mars Environmental Survey (MESUR) Network and Pathfinder Missions

Entry, Descent and Landing Technology Advancement

Interstellar Exploration Through Repeated External Acceleration

Scale: Mars is 6,787 km in diameter. Image 1. What is the feature across the middle? What do you think the circles on the left side are?

Small Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond

GLOBAL CONSTELLATIONS OF STRATOSPHERIC SATELLITES

Facts Largest Moon of Saturn. Has an atmosphere containing mostly Nitrogen and methane. 1 gram on Earth would weigh 0.14g on Titan. Only know moon in

Robotic Mobility Atmospheric Flight

Report of the Venera-D Joint Science Definition Team: "Together to Venus"

LRO Lunar Reconnaissance Orbiter

Lunar Flashlight Project

GLOBAL STRATOSPHERIC BALLOON CONSTELLATIONS

AVIATR: Aerial Vehicle for In situ and Airborne Titan Reconnaissance

ExoMars 2016 Mission

The Main Points. The View from the Surface. Geology of Mars. Lecture #20: Reading:

ASTRIUM. Interplanetary Path Early Design Tools at ASTRIUM Space Transportation. Nathalie DELATTRE ASTRIUM Space Transportation.

A Feasibility Study of a Mars Scout Vehicle to Study Methane

European Venus Explorer

MISSION PROFILE AND DESIGN CHALLENGES FOR MARS LANDING EXPLORATION

Small Entry Probe Trajectories for Mars

GLOBAL CONSTELLATION OF STRATOSPHERIC SCIENTIFIC PLATFORMS

Balloon Concepts for Titan. Ralph D Lorenz, JHU-APL

LOW-COST BALLOON MISSIONS TO MARS AND VENUS

Numerical Simulations of the Mars Science! Laboratory Supersonic Parachute!

Lunar Exploration Requirements and Data Acquisition Architectures

Activity 7 At a Glance

Planetary Surface Processes

Aeolus. A Mission to Map the Winds of Mars. Anthony Colaprete Amanda Cook NASA Ames Research Center

IAA Pre-Summit Conference, Washington, DC, 9 January 2014

Performance Characterization of Supersonic Retropropulsion for Application to High-Mass Mars Entry, Descent, and Landing

InSight Spacecraft Launch for Mission to Interior of Mars

January 11-12, 2007 VEXAG Meeting, Crystal City, VA

Basics of Atomic Hot Air Balloons for Planetary Exploration

Space and Robotics. History of Unmanned Spacecraft David Wettergreen The Robotics Institute Carnegie Mellon University

Expanding Science with SmallSats/CubeSats

Venus Atmosphere Platform Options Reconsidered

Dust in the Atmosphere of Mars 2017 (LPI Contrib. No. 1966)

Titan Saturn System Mission: Jonathan Lunine Co Chair, TSSM JSDT

Activity #1 - Getting Started in Mars Exploration

Ball Aerospace & Technologies Corp. & L Garde Inc.

Deployment of an Interstellar Electromagnetic Acceleration System

Balloon-Based Mars Observation Mission. Final Report. Advanced Design Program. Texas Space Grant Consortium. May 14, 1999

Today s Class. Results for Exam #2 11/7/2017. Today s Class: Robotic & Human Exploration of Mars

Propulsion Technology Assessment: Science and Enabling Technologies to Explore the Interstellar Medium

Mars Exploration Program (MEP) Update

From Celestial North, this is IT S OVER YOUR HEAD for the week of. The New Year brought together revelers the world over for jubilant parties

Mars Sample Return (MSR) Mission BY: ABHISHEK KUMAR SINHA

MODELING OF DUST DEVIL ON MARS AND FLIGHT SIMULATION OF MARS AIRPLANE

1. INTRODUCTION. Gregg Barton Charles Stark Draper Laboratory El Camino Real, Suite 470 Houston, TX

Small Satellite Aerocapture for Increased Mass Delivered to Venus and Beyond

Mission Overview. EAGLE: Study Goals. EAGLE: Science Goals. Mission Architecture Overview

Red Planet Mars. Chapter Thirteen

Paper Session III-B - Mars Global Surveyor: Cruising to Mars

CHARACTERIZATION OF GUIDANCE ALGORITHM PERFORMANCE FOR DRAG MODULATION-BASED AEROCAPTURE

A Lander for Marco Polo

Minimum-Mass Limit of Venus Atmospheric Probes

Missions mars. Beyond the Book. FOCUS Book

The SPE Foundation through member donations and a contribution from Offshore Europe

Introduction of Small Solar Power Sail Demonstrator IKAROS

Six Days at the Edge of Space: 10 Years of HASP Balloon Flight Operations

Titan Saturn System Mission. Jonathan Lunine Co Chair, TSSM JSDT

HERA MISSION & CM16 lessons learned

James L. Green Director, Planetary Science NASA

NASA JPL/NSTA Web Seminar: Robotic Exploration of the Red Planet

IPPW Bio: Robert Dillman BS Aerospace Engineering, University of Virginia 1989; Masters of Materials Science, University of Virginia 1997 NASA

HYBRID AEROCAPTURE USING LOW L/D AEROSHELLS FOR ICE GIANT MISSIONS

Mars 2020 Atmospheric Modeling for Flight Mechanics Simulations

Radio occultation mission to Mars using cubesats

ESA Robotic Science Missions Overview

Mars Entry, Descent, and Landing Parametric Sizing and Design Space Visualization Trades

Economical Surface Balloon Deployment System Concept For Future Scout Class Mars Missions

Deimos and Phobos as Destinations for Human Exploration

LOW-COST LUNAR COMMUNICATION AND NAVIGATION

The Cassini / Huygens Space Mission to Explore the Saturnian System

Venus Bridge: A Smallsat Program Through the Mid-2020s

Surface Observations Including from the 2012 Mars Curiosity Rover. Martian Atmosphere

GEMS: A Revolutionary Concept for Planetary and Space Exploration

ESSE Payload Design. 1.2 Introduction to Space Missions

Lecture #27: Saturn. The Main Point. The Jovian Planets. Basic Properties of Saturn. Saturn:

Weather in the Solar System

E X O M A R S. The ESA/NASA ExoMars Programme

ADVANCES IN GUIDANCE, NAVIGATION, AND CONTROL FOR PLANETARY ENTRY, DESCENT, AND LANDING SYSTEMS

SPRITE: Saturn PRobe Interior and atmosphere Explorer

Transcription:

SAILING THE PLANETS: PLANETARY EXPLORATION FROM GUIDED BALLOONS 7 th Annual Meeting of the NASA Institute for Advanced Concepts DR. ALEXEY PANKINE GLOBAL AEROSPACE CORPORATION SAILING THE PLANETS 1

MARS ROVERS ARE A GREAT SUCCESS Spirit view from Husband Hill summit (NASA/JPL) but their range is very limited SAILING THE PLANETS Columbia Hills surroundings 2 (NASA/JPL/MSSS)

DARE NEW PLATFROM FOR PLANETRAY EXPLORATION An airplane will last for just a few hours Airships propulsion systems make them prohibitively heavy Ordinary balloons are at the mercy of the winds Directed Aerial Robot Explorers (DARE) - guided long-duration balloon platforms Mars Express/ESA-GAC SAILING THE PLANETS 3

NEW ARCHITECTURE FOR PLANETARY EXPLORATION KEY ELEMENTS: Long-Duration Planetary Balloon Platforms Balloon Flight Path Guidance Autonomous Navigation & Control Lightweight Power Generation & Energy Storage Miniaturized Science Sensors Small Deployable Science Packages Communication Relay Orbiter (MTO) Synergy Between Platforms Comprising Architecture SAILING THE PLANETS 4

MARS DARE PLATFORM SCHEMATICS Superpressure balloon (Al top, white paint bottom, D=20-70 m) Gondola: Science payload (~100 kg) Power generation & energy storage Communications Microprobes BGS deployment system (a winch) Tether (5-11 km) Balloon Guidance System (BGS)

DARE ARCHITECTURE APPLICATIONS AND EXPLORATION CAPABILITIES SAILING THE PLANETS 6

EXPLORATION CAPABILITIES Global planetary coverage Heavy, power-intensive payloads (90 kg and 200 W in 3 to 10 years, 170 kg and 400 W >10 years) Long flight duration: 700 days (1 Mars year) Targeted overflight of surface sites and precise delivery of science probes Proximity to surface enables highresolution imaging, elemental, magnetic and gravity surveys not possible or challenging from orbit Olivine outcrop and DS-2 landing ellipse (NASA/JPL/ASU) In situ atmospheric chemistry and circulation Landing sites reconnaissance, navigation beacon emplacement SAILING THE PLANETS Water ice lake inside a crater on Mars 7 (ESA)

FRACTIONATION OF METHANE ISOTOPES IN THE ATMOSPHERE Methane-making organisms discriminate between isotopes as they feed on a global reservoir of CO2 Measure the C 12 /C 13 ratio in the methane. If it is different from the isotope ratio in the CO 2, it would offer strong evidence for a biological source. Tunable Laser Spectrometer for Atmospheric and Sub-surface gas measurements on Mars (NASA JPL) DARE enables planetary-wide search for surface biological sources SAILING THE PLANETS 8

SURFACE TARGETS FOR HIGH- RESOLUTION IMAGING Very small craters Boulders Dichotomy boundary Layers in canyon/crater walls Origins of the outflow channels 10 cm 10 km SAILING THE PLANETS 9

EMPLACEMENT OF SURFACE NETWORKS ON MARS Single DARE platform can carry tens of mini-labs Meteorological & seismological networks Surface labs locations NetLander Surface Module (ESA) Mars Microprobe (NASA) as an example of a mini-lab SAILING THE PLANETS 10

MARS SAMPLE RETURN ASSIST Multiple rovers collect samples at different sites Samples and transferred to Sample Return Vehicle by DARE platform Science results: several samples from distinct sites SAILING THE PLANETS 11

SAILING ACROSS MARTIAN EQUATOR Simulated DARE trajectory over elevation contour map DARE trajectory over MOLA topography (NASA) 90-day late Southern spring, 1 m/s control velocity Objective: navigate from Southern to Northern midlatitudes SAILING THE PLANETS 12

DARE AT VENUS, TITAN, JUPITER VENUS - Targeted overflight of surface sites and precise delivery of geophysical probes - Wind profiles and atmospheric composition at multiple locations TITAN - Global measurements of winds, gas abundances, surface chemistry with probes JUPITER - Solar-Infrared Montgolfier balloons - Sample with probes distinct regions of the atmosphere (Great Red Spot, belt/zone) SAILING THE PLANETS 13

KEY TECHNOLOGIES SAILING THE PLANETS 14

KEY TECHNOLOGIES Three technological time horizons: Current (0-3 years, TRL 8-9), Near (3-10 years, TRL 3-6), Far (beyond 10, TRL 1-3) Advanced Balloon Materials Balloon Guidance System (BGS) Entry, Descent and Inflation (EDI) Navigation & Guidance in Mars winds Mars Balloon performance modeling SAILING THE PLANETS 15

MARS DARE BALLOON Low-mass high-strength envelope material composite material 1-µm Mylar/38-Denier PBO thread/3- µm PE film areal density of 0.012 kg/m 2 Nano-tubes fabric in future? Superpressure sphere Al top, white bottom to prevent CO 2 condensation Mars balloon concept SAILING THE PLANETS Composite Mars balloon material 16

BALLOON GUIDANCE SYSTEM (BGS) BGS is an aerodynamic surface suspended on a tether several km below the balloon Tether could be Zylon fiber, 5 to 20 times stronger than steel, by weight. 10 km long tether weighs 0.5 kg Dual-wing BGS Variation in atmospheric wind and density with altitude result in a sideways lifting force 1 m 2 BGS creates sideways control velocity of 1-2 m/s in typical Martian winds and 8 km tether BGS wing operates at low Reynolds numbers at Mars (~1000), lift coefficients of 0.6-1.4 Single-wing and Dual-wing BGS designs are being studied Single-wing BGS SAILING THE PLANETS 17

ENTRY, DESCENT & INFLATION (EDI) Parachute deploys Inflation commences Parachute cut-off Inflation equipment jettisoned Platform ascends to floating altitude The BGS is deployed Altitude profile SAILING THE PLANETS 18

SYSTEM TRADES AND EXAMPLE DESIGN SAILING THE PLANETS 19

PAYLOAD VS. ALTITUDE Height of atmospheric density levels lower by 4 km in dusty atmosphere DARE to float 2-3 km above southern highlands in dust storm 6 km at τ=3 M=87 kg, R=17.2 m Altitude of 10 km at normal conditions

ALTITUDE CHANGE AFTER PROBE RELEASE Releasing 30 kg of probes raises altitude by 3 km Increase in super-pressure can be relieved by venting 1 kg of gas (out of 8 kg) SAILING THE PLANETS 21

ENTRY VEHICLE Delta 7326 launch rocket, 616 kg Mars injection capability 340 kg Pathfinder-type entry vehicle EDI hardware 200 kg, balloon flight system 140 kg SAILING THE PLANETS 22

BALLOON FLIGHT SYSTEM SAILING THE PLANETS 23

GONDOLA DESIGN SAILING THE PLANETS 24

SUMMARY DARE enables revolutionary planetary exploration capabilities at Mars and other planets DARE addresses NASA's Mars Exploration Program (MEP) goals by returning unique measurements in critical science themes SAILING THE PLANETS 25